Difference between revisions of "Satellite" - New World Encyclopedia

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:''This article is about artificial satellites. For natural satellites, also known as moons, see [[Natural satellite]].''
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:''[[Satellites]] and [[Satalite]] redirect here.  For the Canadian reggae band, see [[Sattalites]].''
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{{otheruses}}
  
[[Image:ERS 2.jpg|thumb|right|300px|An Earth observation satellite, [[ERS 2]]]]
 
In the context of [[spaceflight]], a '''satellite''' is an object which has been placed into [[orbit]] by human endeavor. Such objects are sometimes called '''artificial satellites''' to distinguish them from [[natural satellite]]s such as the [[Moon]].
 
  
==Early theoretical work on artificial satellites ==
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[[Image:ERS 2.jpg|thumb|right|300px|A full size model of the Earth observation satellite [[ERS 2]]]]
The first known fictional depiction of a satellite being launched into orbit is a [[short story]] by [[Edward Everett Hale]], ''[[The Brick Moon]]''. The story was serialized in ''[[The Atlantic Monthly]]'', starting in 1869.<ref>[http://www.gutenberg.org/etext/1633 The Brick Moon and Other Stories by Edward Everett Hale] - Retrieved November 6, 2007.</ref>{{,}}<ref>[http://cdl.library.cornell.edu/cgi-bin/moa/pageviewer?frames=1&cite=http%3A%2F%2Fcdl.library.cornell.edu%2Fcgi-bin%2Fmoa%2Fmoa-cgi%3Fnotisid%3DABK2934-0024-50&coll=moa&view=50&root=%2Fmoa%2Fatla%2Fatla0024%2F&tif=00005.TIF Contents - The Atlantic monthly. Volume 24, Issue 141] - Retrieved November 6, 2007.</ref> The idea surfaces again in [[Jules Verne]]'s [[The Begum's Millions]] (1879).
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In the context of [[spaceflight]], a '''satellite''' is an [[Physical body|object]] which has been placed into [[orbit]] by [[human]] endeavor. Such objects are sometimes called '''artificial satellites''' to distinguish them from [[natural satellite]]s such as the [[Moon]].
  
In 1903 [[Konstantin Tsiolkovsky]] (1857–1935) published Исследование мировых пространств реактивными приборами ''(The Exploration of Cosmic Space by Means of Reaction Devices)'', which is the first academic treatise on the use of rocketry to launch [[spacecraft]]. He calculated the [[orbital speed]] required for a minimal [[orbit]] around the Earth at 8&nbsp;km/second, and that a [[multi-stage rocket]] fueled by liquid [[propellant]]s could be used to achieve this. He proposed the use of [[liquid hydrogen]] and [[liquid oxygen]], though other combinations can be used. During his lifetime he published over 500 works on space travel and related subjects, including science fiction novels. Among his works are designs for rockets with steering thrusters, multi-stage boosters, space stations, airlocks for exiting a spaceship into the vacuum of space, and closed cycle biological systems to provide food and oxygen for space colonies. He also delved into theories of heavier-than-air flying machines, independently working through many of the same calculations that the [[Wright brothers]] were performing at about the same time.
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== History ==
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=== Early conceptions ===
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The first fictional depiction of a satellite being launched into orbit is a [[short story]] by [[Edward Everett Hale]], ''[[The Brick Moon]]''. The story was serialized in ''[[The Atlantic Monthly]]'', starting in 1869.<ref>
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{{cite web|url=http://www.gutenberg.org/etext/1633|title=The Brick Moon and Other Stories by Edward Everett Hale|publisher=[[Project Gutenberg]]|accessdate=2008-03-06}}</ref><ref>
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{{cite web|url=http://cdl.library.cornell.edu/cgi-bin/moa/pageviewer?frames=1&cite=http%3A%2F%2Fcdl.library.cornell.edu%2Fcgi-bin%2Fmoa%2Fmoa-cgi%3Fnotisid%3DABK2934-0024-50&coll=moa&view=50&root=%2Fmoa%2Fatla%2Fatla0024%2F&tif=00005.TIF  |title=Contents - The Atlantic monthly. Volume 24, Issue 141|publisher=cornell.edu|accessdate=2008-03-06}}</ref> The idea surfaces again in [[Jules Verne]]'s [[The Begum's Millions]] (1879).
  
In 1928 [[Herman Potočnik]] (1892–1929) published his sole book, ''Das Problem der Befahrung des Weltraums - der Raketen-Motor'' ''(The Problem of Space Travel—The Rocket Motor)'', a plan for a breakthrough into space and a permanent human presence there. He conceived of a space station in detail and calculated its [[geostationary orbit]]. He described the use of orbiting spacecraft for detailed peaceful and military observation of the ground and described how the special conditions of space could be useful for scientific experiments. The book described geostationary satellites (first put forward by Tsiolkovsky) and discussed communication between them and the ground using radio, but fell short of the idea of using satellites for mass broadcasting and as telecommunications relays.
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In 1903 [[Konstantin Tsiolkovsky]] (1857–1935) published Исследование мировых пространств реактивными приборами (''The Exploration of Cosmic Space by Means of Reaction Devices''), which is the first academic treatise on the use of rocketry to launch [[spacecraft]]. He calculated the [[orbital speed]] required for a minimal [[orbit]] around the Earth at 8&nbsp;km/s, and that a [[multi-stage rocket]] fueled by liquid [[propellant]]s could be used to achieve this. He proposed the use of [[liquid hydrogen]] and [[liquid oxygen]], though other combinations can be used.  
  
In a 1945 ''[[Wireless World]]'' article the English science fiction writer [[Arthur C. Clarke]] (b. 1917) described in detail the possible use of [[communications satellite]]s for mass communications.<ref>[http://www.lsi.usp.br/~rbianchi/clarke/ACC.ETRelaysFull.html Arthur C. Clarke Extra Terrestrial Relays] - Retrieved November 6, 2007.</ref> Clarke examined the logistics of satellite launch, possible [[orbits]] and other aspects of the creation of a network of world-circling satellites, pointing to the benefits of high-speed global communications. He also suggested that three [[geostationary]] satellites would provide coverage over the entire planet.
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In 1928 [[Herman Potočnik]] (1892–1929) published his sole book, ''Das Problem der Befahrung des Weltraums - der Raketen-Motor'' (''The Problem of Space Travel — The Rocket Motor''), a plan for a breakthrough into space and a permanent human presence there. He conceived of a space station in detail and calculated its [[geostationary orbit]]. He described the use of orbiting spacecraft for detailed peaceful and military observation of the ground and described how the special conditions of space could be useful for scientific experiments. The book described geostationary satellites (first put forward by Tsiolkovsky) and discussed communication between them and the ground using radio, but fell short of the idea of using satellites for mass broadcasting and as telecommunications relays.
  
== History of artificial satellites ==
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In a 1945 ''[[Wireless World]]'' article the English science fiction writer [[Arthur C. Clarke]] (1917-2008) described in detail the possible use of [[communications satellite]]s for mass communications.<ref>{{citeweb|title=The_1945_Proposal_by_Arthur_C._Clarke_for_Geostationary_Satellite_Communications|url=http://lakdiva.org/clarke/1945ww/|publisher=lakdiva.org|accessdate=2008-03-06}}</ref> Clarke examined the logistics of satellite launch, possible [[orbits]] and other aspects of the creation of a network of world-circling satellites, pointing to the benefits of high-speed global communications. He also suggested that three [[geostationary]] satellites would provide coverage over the entire planet.
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=== History of artificial satellites ===
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{{Main|Timeline of artificial satellites and space probes}}
 
{{see also | Space Race}}
 
{{see also | Space Race}}
  
The first artificial satellite was [[Sputnik 1]], launched by the [[Soviet Union]] on 4 October 1957. This triggered the [[Space Race]] between the Soviet Union and the [[United States]].
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The first artificial satellite was [[Sputnik 1]], launched by the [[Soviet Union]] on [[4 October]] [[1957]], and that started the whole [[Soviet]] [[Sputnik program]], with [[Sergei Korolev]] as chief designer. This triggered the [[Space Race]] between the [[Soviet Union]] and the [[United States]].
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Sputnik 1 helped to identify the density of high [[Earth's atmosphere#Temperature and the atmospheric layers|atmospheric layers]] through measurement of its orbital change and provided data on [[radio]]-signal distribution in the [[ionosphere]]. Because the satellite's body was filled with pressurized [[nitrogen]], ''Sputnik 1'' also provided the first opportunity for [[meteoroid]] detection, as a loss of internal pressure due to meteoroid penetration of the outer surface would have been evident in the temperature data sent back to Earth. The unanticipated announcement of ''Sputnik 1'''s success precipitated the [[Sputnik crisis]] in the [[United States]] and ignited the so-called [[Space Race]] within the [[Cold War]].
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''[[Sputnik 2]]'' was launched on [[November 3]], [[1957]] and carried the first living passenger into orbit, a [[dog]] named [[Laika]].<ref>{{cite web|title=A Brief History of Animals in Space |publisher=''[[NASA]]'' |url=http://history.nasa.gov/animals.html|accessdate=2007-08-08}}</ref>
  
In May, 1946, [[Project RAND]] had released the [[Preliminary Design of an Experimental World-Circling Spaceship]], which stated, "A satellite vehicle with appropriate instrumentation can be expected to be one of the most potent scientific tools of the Twentieth Century.<ref>[http://www.rand.org/pubs/special_memoranda/SM11827/index.html Preliminary Design of an Experimental Worip] - Retrieved November 6, 2007.</ref>
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In May, 1946, [[Project RAND]] had released the [[Preliminary Design of an Experimental World-Circling Spaceship]], which stated, "A satellite vehicle with appropriate instrumentation can be expected to be one of the most potent scientific tools of the Twentieth Century.<ref>
The [[United States]] had been considering launching [[orbit]]al satellites since 1945 under the [[Bureau of Aeronautics]] of the [[United States Navy]]. The [[United States Air Force]]'s Project RAND eventually released the above report, but did not believe that the satellite was a potential military weapon; rather, they considered it to be a tool for science, politics, and propaganda. In 1954, the Secretary of Defense stated, "I know of no American satellite program."
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{{citeweb|url=http://www.rand.org/pubs/special_memoranda/SM11827/index.html|title=Preliminary Design of an Experimental World-Circling Spaceship|publisher=[[RAND]]|accessdate=2008-03-06}}</ref>
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The [[United States]] had been considering launching [[orbit]]al satellites since 1945 under the [[Bureau of Aeronautics]] of the [[United States Navy]]. The [[United States Air Force]]'s Project RAND eventually released the above report, but did not believe that the satellite was a potential military weapon; rather, they considered it to be a tool for science, politics, and propaganda. In 1954, the Secretary of Defense stated, "I know of no American satellite program."{{Fact|date=May 2008}}
  
On July 29, 1955, the [[White House]] announced that the U.S. intended to launch satellites by the spring of 1958. This became known as [[Project Vanguard]]. On July 31, the Soviets announced that they intended to launch a satellite by the fall of 1957.
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On [[July 29]], [[1955]], the [[White House]] announced that the U.S. intended to launch satellites by the spring of 1958. This became known as [[Project Vanguard]]. On [[July 31]], the Soviets announced that they intended to launch a satellite by the fall of 1957.
  
Following pressure by the [[American Rocket Society]], the [[National Science Foundation]], and the [[International Geophysical Year]], military interest picked up and in early 1955 the Air Force and Navy were working on [[Project Orbiter]], which involved using a [[Jupiter-C IRBM|Jupiter C rocket]] to launch a satellite.  The project succeeded, and [[Explorer 1]] became the United States' first satellite on January 31, 1958.
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Following pressure by the [[American Rocket Society]], the [[National Science Foundation]], and the [[International Geophysical Year]], military interest picked up and in early 1955 the Air Force and Navy were working on [[Project Orbiter]], which involved using a [[Jupiter-C IRBM|Jupiter C rocket]] to launch a satellite.  The project succeeded, and [[Explorer 1]] became the United States' first satellite on [[January 31]], [[1958]].<ref>{{citeweb|title=News Reel - First US Satellite Launched|url= http://www.webcastr.com/videos/news/news-reel-first-us-satellite-launched.html|publisher=webcastr.com|accessdate=2008-03-05}}</ref>
  
 
The largest artificial satellite currently orbiting the Earth is the [[International Space Station]].
 
The largest artificial satellite currently orbiting the Earth is the [[International Space Station]].
  
 
== Space Surveillance Network ==
 
== Space Surveillance Network ==
The [[United States Space Surveillance Network]] (SSN) has been tracking space objects since 1957 when the Soviets opened the space age with the launch of Sputnik I. Since then, the SSN has tracked more than 26,000 space objects orbiting Earth. The SSN currently tracks more than 8,000 man-made orbiting objects. The rest have re-entered Earth's turbulent atmosphere and disintegrated, or survived re-entry and impacted the Earth. The space objects now orbiting Earth range from satellites weighing several tons to pieces of spent rocket bodies weighing only 10 pounds. About seven percent of the space objects are operational satellites (i.e. ~560 satellites), the rest are [[space debris]]. [[USSTRATCOM]] is primarily interested in the active satellites, but also tracks space debris which upon reentry might otherwise be mistaken for incoming missiles. The SSN tracks space objects that are 10 centimeters in diameter (baseball size) or larger.
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The [[United States Space Surveillance Network]] (SSN) has been tracking space objects since 1957 when the Soviets opened the space age with the launch of Sputnik I. Since then, the SSN has tracked more than 26,000 space objects orbiting Earth. The SSN currently tracks more than 8,000 man-made orbiting objects. The rest have re-entered Earth's turbulent atmosphere and disintegrated, or survived re-entry and impacted the Earth. The space objects now orbiting Earth range from satellites weighing several tons to pieces of spent rocket bodies weighing only 10 pounds. About seven percent of the space objects are operational satellites (i.e. ~560 satellites), the rest are [[space debris]].<ref>{{citeweb|title=ORBITAL_DEBRIS_EDUCATION_PACKAGE|url=http://www.orbitaldebris.jsc.nasa.gov/library/EducationPackage.pdf|publisher=nasa.gov|accessdate=2008-03-06}}</ref> [[USSTRATCOM]] is primarily interested in the active satellites, but also tracks space debris which upon reentry might otherwise be mistaken for incoming missiles. The SSN tracks space objects that are 10 centimeters in diameter (baseball size) or larger.
  
 
== Non-Military Satellite Services ==
 
== Non-Military Satellite Services ==
There are three basic categories of non-military satellite services: <ref name="CTU">August E Grant, and Jennifer Harman Meadows. ''Communication Technology Update (ninth edition)''. (Burlington: Focal Press, 2004, ISBN 9780080470320)</ref>
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There are three basic categories of non-military satellite services:<ref name=Grant&Meadows>Grant, A.,& Meadows, J. (2004). Satellites Communication. Communication Technology Update (ninth edition). Burlington: Focal Press.</ref>
  
 
=== Fixed Satellite Service ===
 
=== Fixed Satellite Service ===
Fixed satellite services handle hundreds of millions of voice, data, and video transmission tasks across all continents between fixed points on the earth’s surface
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Fixed satellite services handle hundreds of billions of voice, data, and video transmission tasks across all countries and continents between certain points on the earth’s surface.
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=== Mobile Satellite Systems ===
 
=== Mobile Satellite Systems ===
Mobile satellite systems help connect remote regions, vehicles, ships and aircraft to other parts of the world and/or other mobile or stationary communications units, in addition to serving as navigation systems
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Mobile satellite systems help connect remote regions, vehicles, ships and aircraft to other parts of the world and/or other mobile or stationary communications units, in addition to serving as navigation systems.
  
 
=== Scientific Research Satellite (commercial and noncommercial) ===
 
=== Scientific Research Satellite (commercial and noncommercial) ===
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==Types==
 
==Types==
 
[[Image:Milstar.jpg|thumb|[[MILSTAR]]: A communication satellite]]
 
[[Image:Milstar.jpg|thumb|[[MILSTAR]]: A communication satellite]]
* '''[[Anti-satellite weapon]]s''', sometimes called "Killer satellites" are satellites designed to destroy "enemy" satellites, other orbital weapons and targets. Some are armed with kinetic rounds, while others use energy and/or particle weapons to destroy satellites, ICBMs, MIRVs. Both the U.S. and the USSR had these satellites. Links discussing "Killer satellites," ASATS (Anti-Satellite satellite) include [http://www.jamesoberg.com/pearl.html USSR Tests ASAT weapon] and [http://www.patricksaviation.com/wiki/F-15_ASAT ASAT Test]. See also [[IMINT]]
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*'''[[Anti-Satellite weapons/"Killer Satellites"]]''' are satellites that are armed, designed to take out enemy warheads, satellites, other space assets. They may have particle weapons, energy weapons, kinetic weapons, nuclear and/or conventional missiles and/or a combination of these weapons. In fiction, one has been featured in the movie ''[[Maximum Overdrive]]'' in which one of these, disguised as a "Weather Satellite" had taken out a [[UFO]] with Class IV nuclear weapons and [[laser|laser cannon]].
 
*'''[[Astronomical satellite]]s''' are satellites used for observation of distant planets, galaxies, and other outer space objects.
 
*'''[[Astronomical satellite]]s''' are satellites used for observation of distant planets, galaxies, and other outer space objects.
 
*'''[[Biosatellite]]s''' are satellites designed to carry living organisms, generally for scientific experimentation.
 
*'''[[Biosatellite]]s''' are satellites designed to carry living organisms, generally for scientific experimentation.
 
*'''[[Communications satellite]]s''' are satellites stationed in space for the purpose of [[telecommunications]]. Modern communications satellites typically use [[geosynchronous orbit]]s, [[Molniya orbit]]s or [[Low Earth orbit]]s.
 
*'''[[Communications satellite]]s''' are satellites stationed in space for the purpose of [[telecommunications]]. Modern communications satellites typically use [[geosynchronous orbit]]s, [[Molniya orbit]]s or [[Low Earth orbit]]s.
*'''[[Miniaturized satellites]]''' are satellites of unusually low weights and small sizes. New classifications are used to categorize these satellites: minisatellite (500–200&nbsp;kg), microsatellite (below 200&nbsp;kg), nanosatellite (below 10&nbsp;kg).
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*'''[[Miniaturized satellites]]''' are satellites of unusually low weights and small sizes.<ref>{{citeweb|title=Workshop on the Use of Microsatellite Technologies|url=http://www.unoosa.org/pdf/reports/ac105/AC105_903E.pdf|publisher=[[United Nations]]|accessdate=2008-03-06}}</ref> New classifications are used to categorize these satellites: minisatellite (500–200&nbsp;kg), microsatellite (below 200&nbsp;kg), nanosatellite (below 10&nbsp;kg).
 
*'''[[Global Navigation Satellite System|Navigational satellites]]''' are satellites which use [[radio]] time signals transmitted to enable mobile receivers on the ground to determine their exact location. The relatively clear line of sight between the satellites and receivers on the ground, combined with ever-improving electronics, allows satellite navigation systems to measure location to accuracies on the order of a few meters in real time.
 
*'''[[Global Navigation Satellite System|Navigational satellites]]''' are satellites which use [[radio]] time signals transmitted to enable mobile receivers on the ground to determine their exact location. The relatively clear line of sight between the satellites and receivers on the ground, combined with ever-improving electronics, allows satellite navigation systems to measure location to accuracies on the order of a few meters in real time.
 
*'''[[Reconnaissance satellite]]s''' are [[Earth observation satellite]] or [[communications satellite]] deployed for [[military]] or [[espionage|intelligence]] applications. Little is known about the full power of these satellites, as governments who operate them usually keep information pertaining to their reconnaissance satellites classified.
 
*'''[[Reconnaissance satellite]]s''' are [[Earth observation satellite]] or [[communications satellite]] deployed for [[military]] or [[espionage|intelligence]] applications. Little is known about the full power of these satellites, as governments who operate them usually keep information pertaining to their reconnaissance satellites classified.
*'''[[Earth observation satellite]]s''' are satellites intended for non-military uses such as [[natural environment|environment]]al monitoring, [[meteorology]], [[map making]] etc. (See especially [[Earth Observing System]].)
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*'''[[Earth observation satellite]]s''' are satellites intended for non-military uses such as [[environment (biophysical)|environment]]al monitoring, [[meteorology]], [[map making]] etc. (See especially [[Earth Observing System]].)
*'''[[Space station]]s''' are man-made structures that are designed for [[human|human beings]] to live on in [[outer space]]. A space station is distinguished from other manned [[spacecraft]] by its lack of major [[Spacecraft propulsion|propulsion]] or [[landing]] facilities—instead, other vehicles are used as transport to and from the station. Space stations are designed for medium-term living in [[orbit]], for periods of [[week]]s, [[month]]s, or even [[year]]s.
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*'''[[Space station]]s''' are man-made structures that are designed for [[human|human beings]] to live on in [[outer space]]. A space station is distinguished from other manned [[spacecraft]] by its lack of major [[Spacecraft propulsion|propulsion]] or [[landing]] facilities — instead, other vehicles are used as transport to and from the station. Space stations are designed for medium-term living in [[orbit]], for periods of [[week]]s, [[month]]s, or even [[year]]s.
*'''[[Weather satellite]]s''' are satellites that primarily are used to monitor [[Earth]]'s [[weather]] and [[climate]].
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*'''[[Tether satellite]]s''' are satellites which are connected to another satellite by a thin cable called a [[tether]].
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*'''[[Weather satellite]]s''' are primarily used to monitor [[Earth]]'s [[weather]] and [[climate]].<ref>{{citeweb|title=Earth_Observations_from_Space_The_First_50_Years_of_Scientific_Achievements|url=http://dels.nas.edu/dels/rpt_briefs/earth_observations_final.pdf|publisher=nas.edu|accessdate=2008-03-06}}</ref>
  
 
==Orbit types==
 
==Orbit types==
 
{{main|List of orbits}}
 
{{main|List of orbits}}
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[[Image:Orbits around earth scale diagram.svg|thumb|Various earth orbits to scale; cyan represents low earth orbit, yellow represents medium earth orbit, the black dashed line represents geosynchronous orbit, the green dash-dot line the orbit of [[Global Positioning System]] (GPS) satellites, and the red dotted line the orbit of the [[International Space Station]] (ISS).]]
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The first satellite, [[Sputnik 1]], was put into orbit around [[Earth]] and was therefore in [[geocentric orbit]]. By far this is the most common type of orbit with approximately 2456 artificial satellites orbiting the [[Earth]]. Geocentric orbits may be further classified by their [[altitude]], [[inclination]] and [[Orbital eccentricity|eccentricity]].
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The commonly used altitude classifications are [[Low Earth Orbit]] (LEO), [[Medium Earth Orbit]] (MEO) and [[High Earth Orbit]] (HEO). Low Earth orbit is any orbit below 2000&nbsp;km, and Medium Earth Orbit is any orbit higher than that but still below the altitude for [[geosynchronous orbit]] at 35786&nbsp;km. High Earth Orbit is any orbit higher than the altitude for geosynchronous orbit.
  
 
===Centric classifications===
 
===Centric classifications===
* '''[[Galacto-centric orbit]]''': An orbit about the center of a [[galaxy]]. [[Earth]]'s [[sun]] follows this type of orbit about the [[galactic center]] of the [[Milky Way]].  
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* '''[[galactic center|Galactocentric orbit]]''': An orbit about the center of a [[galaxy]]. [[Earth]]'s [[sun]] follows this type of orbit about the [[galactic center]] of the [[Milky Way]].  
* '''[[Heliocentric orbit]]''': An [[orbit]] around the [[Sun]]. In our [[Solar System]], all [[planets]], [[comets]], and [[asteroids]] are in such orbits, as are many artificial satellites and pieces of [[space debris]]. [[Moons#Moons of the Solar system|Moon]]s by contrast are not in a heliocentric orbit but rather orbit their parent planet.
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* '''[[Heliocentric orbit]]''': An [[orbit]] around the [[Sun]]. In our [[Solar System]], all [[planets]], [[comets]], and [[asteroids]] are in such orbits, as are many artificial satellites and pieces of [[space debris]]. [[Moons#Moons of the Solar system|Moon]]s by contrast are not in a [[heliocentric orbit]] but rather orbit their parent planet.
* '''[[Geocentric orbit]]''': An orbit around the planet [[Earth]], such as the [[Moon]] or [[artificial satellite]]s. Currently there are approximately 2465 artificial satellites orbiting the Earth.
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* '''[[Geocentric orbit]]''': An orbit around the planet [[Earth]], such as the [[Moon]] or [[artificial satellite]]s. Currently there are approximately 2465 artificial satellites orbiting the [[Earth]].
 
* '''[[Areocentric orbit]]''': An orbit around the planet [[Mars]], such as [[Mars moons|moon]]s or [[artificial satellite]]s.
 
* '''[[Areocentric orbit]]''': An orbit around the planet [[Mars]], such as [[Mars moons|moon]]s or [[artificial satellite]]s.
  
 
===Altitude classifications===
 
===Altitude classifications===
 
* '''[[Low Earth Orbit]] (LEO)''': [[Geocentric orbit]]s ranging in altitude from 0–2000 [[km]] (0–1240 [[mile]]s)
 
* '''[[Low Earth Orbit]] (LEO)''': [[Geocentric orbit]]s ranging in altitude from 0–2000 [[km]] (0–1240 [[mile]]s)
* '''[[Medium Earth Orbit]] (MEO)''': [[Geocentric orbit]]s ranging in altitude from 2000 [[km]] (1,240 [[mile]]s) to just below [[geosynchronous orbit]] at 35,786 km (22,240 miles). Also known as an [[intermediate circular orbit]].
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* '''[[Medium Earth Orbit]] (MEO)''': [[Geocentric orbit]]s ranging in altitude from 2000 [[km]] (1240 [[mile]]s) to just below [[geosynchronous orbit]] at 35786 [[km]] (22240 [[mile]]s). Also known as an [[intermediate circular orbit]].
* '''[[High Earth Orbit]] (HEO)''': [[Geocentric orbit]]s above the altitude of [[geosynchronous orbit]] 35,786 [[km]] (22,240 [[mile]]s).
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* '''[[High Earth Orbit]] (HEO)''': [[Geocentric orbit]]s above the altitude of [[geosynchronous orbit]] 35786 [[km]] (22240 [[mile]]s).
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[[Image:Orbitalaltitudes.jpg|thumb|Orbital Altitudes of several significant satellites of earth.]]
  
 
===Inclination classifications===
 
===Inclination classifications===
* '''[[Inclined orbit]]''': An orbit whose [[inclination]] in reference to the [[equatorial plane]] is not 0.  
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* '''[[Inclined orbit]]''': An orbit whose [[inclination]] in reference to the [[equatorial plane]] is not zero degrees.  
 
** '''[[Polar orbit]]''': An [[orbit]] that passes above or nearly above both poles of the planet on each revolution. Therefore it has an [[inclination]] of (or very close to) 90 [[degree (angle)|degree]]s.
 
** '''[[Polar orbit]]''': An [[orbit]] that passes above or nearly above both poles of the planet on each revolution. Therefore it has an [[inclination]] of (or very close to) 90 [[degree (angle)|degree]]s.
** '''Polar [[sun synchronous orbit]]''': A nearly [[polar orbit]] that passes the [[equator]] at the same local time on every pass. Useful for [[image]] taking satellites because [[shadow]]s will be the same on every pass.
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** '''Polar [[sun synchronous orbit]]''': A nearly [[polar orbit]] that passes the [[equator]] at the same local time on every pass. Useful for [[image]] taking satellites because [[shadow]]s will be nearly the same on every pass.
  
 
===Eccentricity classifications===
 
===Eccentricity classifications===
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** '''[[Hohmann transfer orbit]]''': An orbital maneuver that moves a [[spacecraft]] from one [[circular orbit]] to another using two engine [[impulse]]s. This maneuver was named after [[Walter Hohmann]].
 
** '''[[Hohmann transfer orbit]]''': An orbital maneuver that moves a [[spacecraft]] from one [[circular orbit]] to another using two engine [[impulse]]s. This maneuver was named after [[Walter Hohmann]].
 
* '''[[Elliptic orbit]]''': An [[orbit]] with an [[Orbital eccentricity|eccentricity]] greater than 0 and less than 1 whose orbit traces the path of an [[ellipse]].
 
* '''[[Elliptic orbit]]''': An [[orbit]] with an [[Orbital eccentricity|eccentricity]] greater than 0 and less than 1 whose orbit traces the path of an [[ellipse]].
** '''[[Geosynchronous transfer orbit]]''': An [[elliptic orbit]] where the [[perigee]] is at the [[altitude]] of a [[Low Earth Orbit]] (LEO) and the [[apogee]] at the altitude of a [[geosynchronous orbit]].
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** '''[[Geosynchronous transfer orbit]]''': An [[elliptic orbit]] where the [[perigee]] is at the [[altitude]] of a [[Low Earth Orbit]] (LEO) and the [[apogee]] at the [[altitude]] of a [[geosynchronous orbit]].
** '''[[Geostationary transfer orbit]]''': An [[elliptic orbit]] where the [[perigee]] is at the [[altitude]] of a [[Low Earth Orbit]] (LEO) and the [[apogee]] at the altitude of a [[geostationary orbit]].
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** '''[[Geostationary transfer orbit]]''': An [[elliptic orbit]] where the [[perigee]] is at the [[altitude]] of a [[Low Earth Orbit]] (LEO) and the [[apogee]] at the [[altitude]] of a [[geostationary orbit]].
 
** '''[[Molniya orbit]]''': A highly [[elliptic orbit]] with [[inclination]] of 63.4° and [[orbital period]] of half of a [[sidereal day]] (roughly 12 hours). Such a satellite spends most of its time over a designated area of the [[planet]].
 
** '''[[Molniya orbit]]''': A highly [[elliptic orbit]] with [[inclination]] of 63.4° and [[orbital period]] of half of a [[sidereal day]] (roughly 12 hours). Such a satellite spends most of its time over a designated area of the [[planet]].
 
** '''[[Tundra orbit]]''': A highly [[elliptic orbit]] with [[inclination]] of 63.4° and [[orbital period]] of one [[sidereal day]] (roughly 24 hours). Such a satellite spends most of its time over a designated area of the [[planet]].
 
** '''[[Tundra orbit]]''': A highly [[elliptic orbit]] with [[inclination]] of 63.4° and [[orbital period]] of one [[sidereal day]] (roughly 24 hours). Such a satellite spends most of its time over a designated area of the [[planet]].
 
* '''[[Hyperbolic orbit]]''': An [[orbit]] with the eccentricity greater than 1. Such an orbit also has a [[velocity]] in excess of the [[escape velocity]] and as such, will escape the gravitational pull of the [[planet]] and continue to travel [[infinitely]].  
 
* '''[[Hyperbolic orbit]]''': An [[orbit]] with the eccentricity greater than 1. Such an orbit also has a [[velocity]] in excess of the [[escape velocity]] and as such, will escape the gravitational pull of the [[planet]] and continue to travel [[infinitely]].  
* '''[[Parabolic orbit]]''': An [[orbit]] with the eccentricity equal to 1. Such an orbit also has a [[velocity]] equal to the [[escape velocity]] and therefore will escape the gravitational pull of the [[planet]] and travel until its velocity [[Relative motion#Relative motion|relative]] to the planet is 0. If the speed of such an orbit is increased it will become a [[hyperbolic orbit]].
+
* '''[[Parabolic orbit]]''': An [[orbit]] with the eccentricity equal to 1. Such an orbit also has a [[velocity]] equal to the [[escape velocity]] and therefore will escape the gravitational pull of the [[planet]] and travel until its [[velocity]] [[Relative motion#Relative motion|relative]] to the [[planet]] is 0. If the speed of such an orbit is increased it will become a [[hyperbolic orbit]].
 
** '''[[Escape orbit]] (EO)''': A high-speed [[parabolic orbit]] where the object has [[escape velocity]] and is moving away from the [[planet]].
 
** '''[[Escape orbit]] (EO)''': A high-speed [[parabolic orbit]] where the object has [[escape velocity]] and is moving away from the [[planet]].
 
** '''[[Capture orbit]]''': A high-speed [[parabolic orbit]] where the object has [[escape velocity]] and is moving toward the [[planet]].
 
** '''[[Capture orbit]]''': A high-speed [[parabolic orbit]] where the object has [[escape velocity]] and is moving toward the [[planet]].
Line 88: Line 109:
 
===Synchronous classifications===
 
===Synchronous classifications===
 
* '''[[Synchronous orbit]]''': An orbit where the satellite has an [[orbital period]] equal to the average [[rotational period]] (earth's is: 23 [[hour]]s, 56 [[minute]]s, 4.091 [[second]]s) of the body being orbited and in the same direction of rotation as that body.  To a ground observer such a satellite would trace an [[analemma]] (figure 8) in the sky.  
 
* '''[[Synchronous orbit]]''': An orbit where the satellite has an [[orbital period]] equal to the average [[rotational period]] (earth's is: 23 [[hour]]s, 56 [[minute]]s, 4.091 [[second]]s) of the body being orbited and in the same direction of rotation as that body.  To a ground observer such a satellite would trace an [[analemma]] (figure 8) in the sky.  
* '''[[Semi-synchronous orbit]] (SSO)''': An [[orbit]] with an [[altitude]] of approximately 20,200 km (12544.2 miles) and an [[orbital period]] of approximately 12 hours
+
* '''[[Semi-synchronous orbit]] (SSO)''': An [[orbit]] with an [[altitude]] of approximately 20200 km (12544.2 miles) and an [[orbital period]] equal to one-half of the average [[rotational period]] (earth's is approximately 12 hours) of the body being orbited
* '''[[Geosynchronous orbit]] (GEO)''': Orbits with an altitude of approximately 35,786 km (22,240 miles). Such a satellite would trace an [[analemma]] (figure 8) in the sky.
+
* '''[[Geosynchronous orbit]] (GEO)''': Orbits with an altitude of approximately 35786 km (22240 miles). Such a satellite would trace an [[analemma]] (figure 8) in the sky.
** '''[[Geostationary orbit]] (GSO)''': A [[geosynchronous orbit]] with an [[inclination]] of zero. To an observer on the ground this satellite would appear as a fixed point in the sky.
+
** '''[[Geostationary orbit]] (GSO)''': A [[geosynchronous orbit]] with an [[inclination]] of zero. To an observer on the ground this satellite would appear as a fixed point in the sky.<ref>{{citeweb|title=PEARL HARBOR IN SPACE|url=http://www.jamesoberg.com/pearl.html|publisher=jamesoberg.com|accessdate=2008-03-06}}</ref>
*** '''[[Clarke orbit]]''': Another name for a [[geostationary orbit]]. Named after the writer [[Arthur C. Clarke]].  
+
*** '''[[Clarke orbit]]''': Another name for a [[geostationary orbit]]. Named after scientist and writer [[Arthur C. Clarke]].  
 
** '''[[Supersynchronous orbit]]''': A disposal / storage orbit above GSO/GEO. Satellites will drift west.  Also a [[synonym]] for Disposal orbit.
 
** '''[[Supersynchronous orbit]]''': A disposal / storage orbit above GSO/GEO. Satellites will drift west.  Also a [[synonym]] for Disposal orbit.
 
** '''[[Subsynchronous orbit]]''': A drift orbit close to but below GSO/GEO. Satellites will drift east.
 
** '''[[Subsynchronous orbit]]''': A drift orbit close to but below GSO/GEO. Satellites will drift east.
Line 97: Line 118:
 
*** '''[[Disposal orbit]]''': A [[synonym]] for [[graveyard orbit]].
 
*** '''[[Disposal orbit]]''': A [[synonym]] for [[graveyard orbit]].
 
*** '''[[Junk orbit]]''': A [[synonym]] for [[graveyard orbit]].
 
*** '''[[Junk orbit]]''': A [[synonym]] for [[graveyard orbit]].
* '''[[Areosynchronous orbit]]''': A [[synchronous orbit]] around the planet [[Mars]] with an [[orbital period]] equal in length to Mars' [[sidereal day]], 24.6229 [[hours]].  
+
* '''[[Areosynchronous orbit]]''': A [[synchronous orbit]] around the planet [[Mars]] with an [[orbital period]] equal in length to Mars' [[sidereal day]], 24,6229 [[hours]].  
* '''[[Areostationary orbit]] (ASO)''': A [[circular]] [[areosynchronous orbit]] on the [[equatorial plane]] and about 17,000 [[km]](10557 [[mile]]s)  above the surface. To an observer on the ground this satellite would appear as a fixed point in the sky.
+
* '''[[Areostationary orbit]] (ASO)''': A [[circular]] [[areosynchronous orbit]] on the [[equatorial plane]] and about 17000 [[km]](10557 [[mile]]s)  above the surface. To an observer on the ground this satellite would appear as a fixed point in the sky.
* '''[[Heliosynchronous orbit]]''': An [[heliocentric orbit]] about the [[Sun]] where the satellite's [[orbital period]] matches the Sun's period of [[rotation]]. These orbits occur at a radius of 24.360 [[gigametre|Gm]] (0.1628 [[AU]]) around the Sun, a little less than half of the [[orbital radius]] of [[Mercury (planet)|Mercury]].
+
* '''[[Heliosynchronous orbit]]''': An [[heliocentric orbit]] about the [[Sun]] where the satellite's [[orbital period]] matches the [[Sun]]'s period of [[rotation]]. These orbits occur at a radius of 24,360 [[gigametre|Gm]] (0,1628 [[AU]]) around the [[Sun]], a little less than half of the [[orbital radius]] of [[Mercury (planet)|Mercury]].
  
 
===Special classifications===
 
===Special classifications===
 
* '''[[Sun-synchronous orbit]]''': An orbit which combines [[altitude]] and [[inclination]] in such a way that the satellite passes over any given point of the [[planets]]'s surface at the same local [[solar time]]. Such an orbit can place a satellite in constant sunlight and is useful for [[imaging]], [[spy satellite|spy]], and [[weather satellite]]s.
 
* '''[[Sun-synchronous orbit]]''': An orbit which combines [[altitude]] and [[inclination]] in such a way that the satellite passes over any given point of the [[planets]]'s surface at the same local [[solar time]]. Such an orbit can place a satellite in constant sunlight and is useful for [[imaging]], [[spy satellite|spy]], and [[weather satellite]]s.
* '''[[Moon orbit]]''': The [[Orbital parameters|orbital characteristics]] of [[earth]]'s [[moon]]. Average [[altitude]] of 384,403 kilometres (238,857 mi), [[elliptical orbit|elliptical]]-[[inclined orbit]].
+
* '''[[Moon orbit]]''': The [[Orbital parameters|orbital characteristics]] of [[earth]]'s [[moon]]. Average [[altitude]] of 384403 kilometres (238857 mi), [[elliptical orbit|elliptical]]-[[inclined orbit]].
  
 
=== Pseudo-orbit classifications ===
 
=== Pseudo-orbit classifications ===
* '''[[Horseshoe orbit]]''': An [[orbit]] that appears to a ground observer to be orbiting a certain  [[planet]] but is actually in [[Co-orbital satellite|co-orbit]] with the planet. See asteroids [[3753 Cruithne|3753]] (Cruithne) and [[2002 AA29|2002 AA<small><sub>29</sub></small>]].
+
* '''[[Horseshoe orbit]]''': An [[orbit]] that appears to a ground observer to be orbiting a certain  [[planet]] but is actually in [[Co-orbital satellite|co-orbit]] with the [[planet]]. See asteroids [[3753 Cruithne|3753]] (Cruithne) and [[2002 AA29|2002 AA<small><sub>29</sub></small>]].
 
* '''[[Exo-orbit]]''': A maneuver where a [[spacecraft]] approaches the height of [[orbit]] but lacks the [[velocity]] to sustain it.   
 
* '''[[Exo-orbit]]''': A maneuver where a [[spacecraft]] approaches the height of [[orbit]] but lacks the [[velocity]] to sustain it.   
** '''[[Orbital spaceflight]]''': A [[synonym]] for [[exo-orbit]].
+
** '''[[Suborbital spaceflight]]''': A [[synonym]] for [[exo-orbit]].
 
* '''[[Lunar transfer orbit]] (LTO)'''
 
* '''[[Lunar transfer orbit]] (LTO)'''
 
* '''[[Prograde orbit]]''': An [[orbit]] with an inclination of less than 90°. Or rather, an orbit that is in the same direction as the rotation of the primary.
 
* '''[[Prograde orbit]]''': An [[orbit]] with an inclination of less than 90°. Or rather, an orbit that is in the same direction as the rotation of the primary.
* '''[[Retrograde orbit]]''': An [[orbit]] with an [[inclination]] of more than 90°. Or rather, an orbit counter to the direction of rotation of the planet.  Apart from those in [[sun-synchronous orbit]], few satellites are launched into retrograde orbit because the quantity of fuel required to launch them is much greater than for a [[prograde orbit]]. This is because when the rocket starts out on the ground, it already has an eastward component of [[velocity]] equal to the rotational velocity of the planet at its launch [[latitude]].
+
* '''[[Retrograde orbit]]''': An [[orbit]] with an [[inclination]] of more than 90°. Or rather, an orbit counter to the direction of rotation of the planet.  Apart from those in [[sun-synchronous orbit]], few satellites are launched into [[retrograde orbit]] because the quantity of fuel required to launch them is much greater than for a [[prograde orbit]]. This is because when the rocket starts out on the ground, it already has an eastward component of [[velocity]] equal to the rotational velocity of the planet at its launch [[latitude]].
 
+
*'''[[Halo orbit]]''' and '''[[Lissajous orbit]]''': Orbits "around" [[Lagrangian point]]s.
Satellites can also orbit [[Lagrangian point]]s.
 
  
 
== Satellite Modules ==
 
== Satellite Modules ==
The satellite’s functional versatility is imbedded within its technical components and its operations characteristics. Looking at the “anatomy” of a satellite, one discover two modules. <ref name="CTU"/>
+
The satellite’s functional versatility is imbedded within its technical components and its operations characteristics. Looking at the “anatomy” of a typical satellite, one discovers two modules.<ref name=Grant&Meadows/> Note that some novel architectural concepts such as [[Fractionated Spacecraft]] somewhat upset this taxonomy.
  
 
=== Spacecraft bus or service module ===  
 
=== Spacecraft bus or service module ===  
This first module consist of five subsystems :
+
This first module consist of five subsystems:
* '''[[The Structural Subsystem]]s'''
+
* '''The Structural Subsystems'''
The structural subsystem provides the mechanical base structure, shields the satellite from extreme temperature changes and micro-meteorite damage, and controls the satellite’s spin functions.
+
The structural subsystem provides the mechanical base structure, shields the satellite from extreme temperature changes and micro-meteorite damage, and controls the satellite’s spin functions.
* '''[[The Telemetry Subsystem]]s'''
+
* '''The Telemetry Subsystems'''
 
The telemetry subsystem  monitors the on-board equipment operations, transmits equipment operation data to the earth control station, and receives the earth control station’s commands to perform equipment operation adjustments.
 
The telemetry subsystem  monitors the on-board equipment operations, transmits equipment operation data to the earth control station, and receives the earth control station’s commands to perform equipment operation adjustments.
* '''[[The Power Subsystem]]s'''
+
* '''The Power Subsystems'''
The power subsystem is comprised of solar panel and backup batteries that generate power when the satellite passes into the earth’s shadow.
+
The power subsystem consists of solar panels and backup batteries that generate power when the satellite passes into the earth’s shadow.
* '''[[The Thermal Control Subsystem]]s
+
* '''The Thermal Control Subsystems
 
The thermal control subsystem helps protect electronic equipment from extreme temperatures due to intense sunlight or the lack of sun exposure on different sides of the satellite’s body
 
The thermal control subsystem helps protect electronic equipment from extreme temperatures due to intense sunlight or the lack of sun exposure on different sides of the satellite’s body
* '''[[The Altitude and Orbit Controlled Control Subsystem]]s
+
* '''The Attitude and Orbit Controlled Control Subsystems
The altitude and orbit controlled subsystem is comprised of small rocket thursters that keep the satellite in the correct orbital position and keep antennas positioning in the right directions.
+
The attitude and orbit controlled subsystem consists of small rocket thrusters that keep the satellite in the correct orbital position and keep antennas positioning in the right directions.
  
 
=== Communication Payload ===
 
=== Communication Payload ===
 
The second major module is the communication payload, which is made up of transponders. A transponders is capable of :
 
The second major module is the communication payload, which is made up of transponders. A transponders is capable of :
* '''[[Receiving uplinked radio signals from earth satellite transmission stations (antennas).]]
+
* '''Receiving uplinked radio signals from earth satellite transmission stations (antennas).
* '''[[Amplifying received radio signals]]
+
* '''Amplifying received radio signals
* '''[[Sorting the input signals and directing the output signals through input/output signal multiplexers to the proper downlink antennas for retransmission to earth satellite receiving stations (antennas).]]
+
* '''Sorting the input signals and directing the output signals through input/output signal multiplexers to the proper downlink antennas for retransmission to earth satellite receiving stations (antennas).
  
==Launch-capable countries==
+
==Launch-capable countries ==
 
{{main|Timeline of first orbital launches by nationality}}
 
{{main|Timeline of first orbital launches by nationality}}
This list includes countries with an independent capability to place satellites in orbit, including production of the necessary launch vehicle. Note: many more countries have the capability to design and build satellites—which relatively speaking, does not require much economic, scientific and industrial capacity—but are unable to launch them, instead relying on foreign launch services.  This list '''does not''' consider those numerous countries, but only lists those capable of launching satellites indigenously, and the date this capability was first demonstrated.  Does not include consortium satellites or multi-national satellites.
+
[[Image:Delta-M with Skynet-1A.jpg|thumb|right|Launch of the first [[United Kingdom|British]] [[Skynet (satellites)|Skynet]] military satellite.]]
 +
This list includes countries with an independent capability to place satellites in orbit, including production of the necessary launch vehicle. Note: many more countries have the capability to design and build satellites — which relatively speaking, does not require much economic, scientific and industrial capacity — but are unable to launch them, instead relying on foreign launch services.  This list '''does not''' consider those numerous countries, but only lists those capable of launching satellites indigenously, and the date this capability was first demonstrated.  Does not include consortium satellites or multi-national satellites.
  
 
{| class="sortable wikitable"
 
{| class="sortable wikitable"
 
|+ '''First launch by country'''
 
|+ '''First launch by country'''
 
|- bgcolor=#efefef
 
|- bgcolor=#efefef
! Country || Year of first launch || First satellite || Launches to orbit in 2006<ref name="boxscore">[http://www.celestrak.com/satcat/boxscore.asp CelesTrak WWW: SATCAT Boxscore] - Retrieved November 6, 2007.</ref>
+
! Country || Year of first launch || First satellite
 
|-
 
|-
|align="left"| {{flag|Soviet Union}}<br/>{{flag|Russia}}<br/>{{flag|Ukraine}} || 1957 || ''[[Sputnik 1]]'' || 1390
+
|align="left"| {{flag|Soviet Union}} || 1957 || ''[[Sputnik 1]]''  
 
|-
 
|-
|align="left"| {{flag|United States}} || 1958 || ''[[Explorer 1]]'' || 999
+
|align="left"| {{flag|United States}} || 1958 || ''[[Explorer 1]]''  
 
|-
 
|-
|align="left"| {{flag|France}} || 1965 || ''[[Astérix (satellite)|Astérix]]'' || 43
+
|align="left"| {{flag|France}} || 1965 || ''[[Astérix (satellite)|Astérix]]''  
 
|-
 
|-
|align="left"| {{flag|Australia}} || 1967 || ''[[WRESAT]]'' || 1
+
|align="left"| {{flag|Japan}} || 1970 || ''[[Osumi (Satellite)|Osumi]]''  
 
|-
 
|-
|align="left"| {{flag|Japan}} || 1970 || ''[[Osumi (Satellite)|Osumi]]'' || 102
+
|align="left"| {{flag|China}} || 1970 || ''[[Dong Fang Hong I]]''  
 
|-
 
|-
|align="left"| {{flag|China}} || 1970 || ''[[Dong Fang Hong I]]'' || 53
+
|align="left"| {{flag|United Kingdom}} || 1971 || ''[[Prospero X-3]]''
 
|-
 
|-
|align="left"| {{flag|United Kingdom}} || 1971 || ''[[Prospero X-3]]'' || 23{{Fact|date=February 2007}}<!--Britain stopped launching spacecraft after Prospero.—>
+
|align="left"| {{flag|India}} || 1980 || ''[[Rohini space satellite|Rohini]]''  
 
|-
 
|-
|align="left"| {{flag|India}} || 1981 || ''[[Rohini space satellite|Rohini]]'' || 31
+
|align="left"| {{flag|Israel}} || 1988 ||''[[Ofeq|Ofeq 1]]''  
|-
 
|align="left"| {{flag|Israel}} || 1988 ||''[[Ofeq|Ofeq 1]]'' || 6
 
 
|}
 
|}
 
<!-- Please do not add Kazakhstan, see below, and on talk page for details —>
 
<!-- Please do not add Kazakhstan, see below, and on talk page for details —>
  
Both [[North Korea]] (1998) and [[Iraq]] (1989) have claimed orbital launches, but these claims are unconfirmed.   
+
Both [[North Korea]] (1998) and [[Iraq]] (1989) have claimed orbital launches (satellite and warhead accordingly), but these claims are unconfirmed.   
 
 
In addition to the above, countries such as [[South Africa]], [[Spain]], [[Italy]], [[West Germany]], [[Canada]], [[Australia]], [[Argentina]], [[Egypt]], and private companies such as [[OTRAG]], have developed their own launchers, but have not had a successful launch.
 
  
[[As of 2007]], only seven countries from list above (six 'major'—[[Russia]] and [[Ukraine]] instead of [[USSR]], also [[USA]], [[Japan]], [[China]], [[India]], and one 'minor'—[[Israel]]) and one regional organization (the [[European Union]], represented by [[European Space Agency]], ESA) have independently launched satellites on their own indigenously developed launch vehicles. (The launch capabilities of the [[United Kingdom]] and [[France]] now fall under the [[ESA]].)
+
In addition to the above, countries such as [[South Africa]], [[Spain]], [[Italy]], [[West Germany]], [[Canada]], [[Australia]], [[Argentina]], [[Egypt]] and private companies such as [[OTRAG]], have developed their own launchers, but have not had a successful launch.
  
Also, one international private company ([[Sea Launch]]) has launch capability through their purchase of Ukrainian–Russian launchers.
+
As of 2008, only seven countries from list above ( [[Russia]] and [[Ukraine]] instead of [[USSR]], also [[USA]], [[Japan]], [[China]], [[India]], and [[Israel]]) and one regional organization (the [[European Space Agency]], ESA) have independently launched satellites on their own indigenously developed launch vehicles. (The launch capabilities of the [[United Kingdom]] and [[France]] now fall under the [[ESA]].)
  
Several other countries, including [[Brazil]], [[Iran]], [[South Korea]], [[Malaysia]], [[Pakistan]], and [[Turkey]], are at various stages of development of their own small-scale launcher capabilities, and seek membership in the club of space powers.
+
Several other countries, including [[South Korea]], [[Iran]], [[Brazil]], [[Pakistan]], [[Romania]], [[Kazakhstan]], [[Australia]], [[Malaysia]]{{Fact|date=June 2008}} and [[Turkey]], are at various stages of development of their own small-scale launcher capabilities, and seek membership in the club of space powers.
  
[[KARI|South Korea]], with assistance with [[Russia]] is building [[Korea Space Center]] in [[Goheung]], [[Jeolla Province]]. It is schedule to be operating in early 2008, and South Korea is launching [[KSLV]] rocket to put the nation's satellite up into space.  
+
It is scheduled that in early 2008 [[Korea Aerospace Research Institute|South Korea]] will launch a [[KSLV]] rocket (created with assistance of Russia) and become the next space power. [[Iran]] already has successfully tested its own space launch vehicle ([[Kavoshgar 1]]) and is scheduled to put its first domestic satellite ([[Omid (satellite)|Omid 1]]) into orbit within a year from [[February 4]] [[2008]]. It is expected that Brazil and Pakistan will follow in the near future..{{Fact|date=May 2008}}
  
 
{| class="sortable wikitable"
 
{| class="sortable wikitable"
|+ '''First launch by country including help of other parties'''
+
|+ '''First launch by country including help of other parties'''<ref>{{citeweb|title=First time in History|url=http://www.tbs-satellite.com/tse/online/thema_first.html|publisher=tbs-satellite.com|accessdate=2008-03-06}}</ref>
 
|- bgcolor=#efefef
 
|- bgcolor=#efefef
! Country || Year of first launch || First satellite || Payloads in orbit in 2006<ref name="boxscore"/>
+
! Country || Year of first launch || First satellite || Payloads in orbit in 2008<ref>{{citeweb|title=SATCAT Boxscore|url=http://www.celestrak.com/satcat/boxscore.asp|publisher=celestrak.com|accessdate=2008-03-05}}</ref>
 +
|-
 +
|align="left"| {{flag|Soviet Union}} || 1957 || ''[[Sputnik 1]]'' || 1398
 +
|-
 +
|align="left"| {{flag|United States}} || 1958 || ''[[Explorer 1]]'' || 1042
 +
|-
 +
|align="left"| {{flag|Canada}} || 1962 || ''[[Alouette 1]]'' || 25
 +
|-
 +
|align="left"| {{flag|Italy}} || 1964 || ''[[San Marco 1]]'' ||14
 +
|-
 +
|align="left"| {{flag|France}} || 1965 || ''[[Astérix (satellite)|Astérix]]'' || 44
 +
|-
 +
|align="left"| {{flag|Australia}} || 1967 || ''[[WRESAT]]'' || 11
 
|-
 
|-
|align="left"| {{flag|Soviet Union}}<br/>{{flag|Russia}}<br/>{{flag|Ukraine}} || 1957 || ''[[Sputnik 1]]'' || 1390
+
|align="left"| {{flag|Germany}} || 1969 || ''[[Azur (satellite)|Azur]]'' ||27
 
|-
 
|-
|align="left"| {{flag|United States}} || 1958 || ''[[Explorer 1]]'' || 999
+
|align="left"| {{flag|Japan}} || 1970 || ''[[Osumi (Satellite)|Osumi]]'' || 111
 
|-
 
|-
|align="left"| {{flag|Canada}} || 1962 || ''[[Alouette 1]]'' || 33
+
|align="left"| {{flag|China}} || 1970 || ''[[Dong Fang Hong I]]'' || 64
 
|-
 
|-
|align="left"| {{flag|Italy}} || 1964 || ''[[San Marco 1]]'' ||  
+
|align="left"| {{flag|United Kingdom}} || 1971 || ''[[Prospero X-3]]'' || 25
 
|-
 
|-
|align="left"| {{flag|France}} || 1965 || ''[[Astérix (satellite)|Astérix]]'' || 43
+
|align="left"| {{flag|Poland}} || 1973 || ''[[Intercosmos#Unmanned_missions|Intercosmos Kopernikus 500]]'' || ?
 
|-
 
|-
|align="left"| {{flag|Australia}} || 1967 || ''[[WRESAT]]'' ||  
+
|align="left"| {{flag|Netherlands}} || 1974 || ''[[ANS (satellite)|ANS]]'' || 5
 
|-
 
|-
|align="left"| {{flag|Japan}} || 1970 || ''[[Osumi (Satellite)|Osumi]]'' || 102
+
|align="left"| {{flag|Spain}} || 1974 || ''[[Intasat]]'' || 9
 
|-
 
|-
|align="left"| {{flag|China}} || 1970 || ''[[Dong Fang Hong I]]'' || 53
+
|align="left"| {{flag|India}} || 1975 || ''[[Aryabhata (satellite)|Aryabhata]]'' || 34
 
|-
 
|-
|align="left"| {{flag|United Kingdom}} || 1971 || ''[[Prospero X-3]]'' || 23
+
|align="left"| {{flag|Indonesia}} || 1976 || ''[[Palapa#Series_A|Palapa A1]]'' ||10
 
|-
 
|-
|align="left"| {{flag|India}} || 1975 || ''[[Aryabhata (satellite)|Aryabhata]]'' || 31
+
|align="left"| {{flag|Czechoslovakia}} || 1978 || ''[[Magion 1]]'' || 5
 
|-
 
|-
|align="left"| {{flag|Israel}} || 1988 ||''[[Ofeq|Ofeq 1]]'' || 6
+
|align="left"| {{flag|Bulgaria}} || 1981 || ''[[Intercosmos#Unmanned_missions|Intercosmos 22]]'' ||  
 
|-
 
|-
|align="left"| {{flag|Portugal}} || 1993 ||''[[PoSAT-1]]'' ||  
+
|align="left"| {{flag|Brazil}} || 1985 || ''[[Brasilsat A1]]'' ||11
 
|-
 
|-
|align="left"| {{flag|Egypt}} || 1998||''[[NileSat 101]]'' || 3
+
|align="left"| {{flag|Mexico}} || 1985 || ''[[Morelos 1]]'' || 7
 +
|-
 +
|align="left"| {{flag|Sweden}} || 1986 || ''[[Viking (satellite)|Viking]]'' || 11
 +
|-
 +
|align="left"| {{flag|Israel}} || 1988 ||''[[Ofeq|Ofeq 1]]'' || 7
 +
|-
 +
|align="left"| {{flag|Luxembourg}} || 1988 ||''[[Astra 1A]]'' ||15
 +
|-
 +
|align="left"| {{flag|Argentina}} || 1990 ||''[[Lusat]]'' || 10
 +
|-
 +
|align="left"| {{flag|Pakistan}} || 1990 ||''[[Badr-1]]'' ||5
 +
|-
 +
|align="left"| {{flag|South Korea}} || 1992 ||''[[Kitsat A]]'' ||10
 +
|-
 +
|align="left"| {{flag|Portugal}} || 1993 ||''[[PoSAT-1]]'' || 1
 +
|-
 +
|align="left"| {{flag|Thailand}} || 1993 ||''[[Thaicom|Thaicom 1]]'' || 6
 +
|-
 +
|align="left"| {{flag|Turkey}} || 1994 ||''[[Turksat 1B]]'' || 5
 +
|-
 +
|align="left"| {{flag|Chile}} || 1995 ||''[[FASat-Alfa]]'' ||1
 +
|-
 +
|align="left"| {{flag|Malaysia}} || 1996 ||''[[MEASAT]]'' ||4
 +
|-
 +
|align="left"| {{flag|Norway}} || 1997 ||''[[Thor 2]]'' ||3
 +
|-
 +
|align="left"| {{flag|Philippines}} || 1997 ||''[[Mabuhay 1]]'' ||2
 +
|-
 +
|align="left"| {{flag|Egypt}} || 1998||''[[Nilesat 101]]'' || 3
 +
|-
 +
|align="left"| {{flag|Denmark}} || 1999 ||''[[Ørsted (satellite)|Ørsted]]'' ||3
 +
|-
 +
|align="left"| {{flag|South Africa}} || 1999||''[[SUNSAT]]'' ||1
 +
|-
 +
|align="left"| {{flag|Saudi Arabia}} || 2000||''[[Saudisat 1A]]'' || 12
 +
|-
 +
|align="left"| {{flag|United Arab Emirates}} || 2000||''[[Thuraya#Satellites|Thuraya 1]]'' ||3
 +
|-
 +
|align="left"| {{flag|Algeria}} || 2002||''[[Alsat 1]]'' ||1
 +
|-
 +
|align="left"| {{flag|Greece}} || 2003||''[[Hellas Sat 2]]'' || 2
 +
|-
 +
|align="left"| {{flag|Nigeria}} || 2003||''[[Nigeriasat 1]]'' ||2
 
|-
 
|-
 
|align="left"| {{flag|Iran}} || 2005 || ''[[Sina-1]]'' || 1
 
|align="left"| {{flag|Iran}} || 2005 || ''[[Sina-1]]'' || 1
 
|-
 
|-
 
|align="left"| {{flag|Kazakhstan}} || 2006 || ''[[KazSat|KazSat 1]]'' || 1
 
|align="left"| {{flag|Kazakhstan}} || 2006 || ''[[KazSat|KazSat 1]]'' || 1
 +
|-
 +
|align="left"| {{flag|Colombia}} || 2007 || ''[[Libertad 1]]'' ||1
 +
|-
 +
|align="left"| {{flag|Vietnam}} || 2008 || ''[[VINASAT-1]]'' ||1
 
|}
 
|}
  
While [[Canada]] was the third country to build a satellite which was launched into Space, it was launched aboard a U.S. rocket from a U.S. spaceport.  The same goes for [[Australia]], who launched on-board a donated Redstone rocket. The first Italian-launched was [[San Marco 1]], launched on 15 December, 1964 on a U.S. [[Scout rocket]] from Wallops Island (VA,USA) with an Italian Launch Team trained by NASA.<ref>[http://nssdc.gsfc.nasa.gov/database/MasterCatalog?sc=1964-084A NSSDC Master Catalog Display: Spacecraft] - Retrieved November 6, 2007.</ref>. Australia's launch project, in November 1967, involved a donated U.S. missile and U. S. support staff as well as a joint launch facility with the [[United Kingdom]].<ref>[http://homepage.powerup.com.au/~woomera/wresat.htm WRESAT] - Retrieved November 6, 2007.</ref> [[Kazakhstan]] claimed to have launched their satellite independently, but the satellite was built with Russian help.
+
While [[Canada]] was the third country to build a satellite which was launched into space,<ref>{{citeweb|title=Canada's Churchill Spaceport|url=http://www.spacetoday.org/Rockets/Spaceports/Canada.html|publisher=spacetoday.org|accessdate=2008-03-06}}</ref> it was launched aboard a U.S. rocket from a U.S. spaceport.  The same goes for [[Australia]], who launched on-board a donated Redstone rocket. The first Italian-launched was [[San Marco 1]], launched on [[15 December]], [[1964]] on a U.S. [[Scout rocket]] from Wallops Island (VA,USA) with an Italian Launch Team trained by NASA.<ref>{{citeweb|title=San Marco 1|url=http://nssdc.gsfc.nasa.gov/database/MasterCatalog?sc=1964-084A|publisher=nasa.gov|accessdate=2008-03-05}}</ref> [[Australia]]'s launch project, in November 1967, involved a donated U.S. missile and U. S. support staff as well as a joint launch facility with the [[United Kingdom]].<ref>{{citeweb|title=WRESAT_Australia's_First_Satellite|url=http://homepage.powerup.com.au/~woomera/wresat.htm|publisher=powerup.com.au|accessdate=2008-03-05}}</ref> [[Kazakhstan]] claimed to have made their satellite independently{{Fact|date=May 2008}}, but the satellite was built with Russian help, like Polish and Bulgarian ones earlier.
  
==Heraldry==
+
==Attacks on satellites==
The (artificial, though this is not stated in the blazon) satellite appears as a [[charge (heraldry)|charge]] in the arms of [[Arthur Maxwell House]].<ref>[http://heraldry.ca/arms/h/house.htm Arms of the House family] - Retrieved November 6, 2007.</ref> This is in addition to numerous appearances of the natural satellite the [[moon]], and the moons of the [[planet]]s [[Jupiter (planet)|Jupiter]] and [[Saturn (planet)|Saturn]] (with those planets) in the arms of [[Pierre Laplace|Pierre-Simon LaPlace]].
+
{{ Details|Anti-satellite weapon }}
 +
 
 +
In recent times satellites have been hacked by militant organisations to broadcast propaganda and to pilfer classified information from military communication networks.<ref>{{citeweb|title=Hack a Satellite while it is in orbit|url=http://blogs.ittoolbox.com/security/dmorrill/archives/hack-a-satellite-while-it-is-in-orbit-15690|publisher=ittoolbox.com|accessdate=2008-03-25}}</ref><ref>{{citeweb|title=AsiaSat accuses Falungong of hacking satellite signals|url=http://www.accessmylibrary.com/coms2/summary_0286-5205866_ITM|publisher=[[Press Trust of India]]|accessdate=2008-03-25}}</ref>
 +
 
 +
Satellites in low earth orbit have been destroyed by ballistic missiles launched from earth. Both [[Russia]] and the [[United States]] have demonstrated ability to eliminate satellites.<ref name="asat">{{citeweb|title=China Tests Anti-Satellite Weapon, Unnerving U.S.|url=http://www.nytimes.com/2007/01/18/world/asia/18cnd-china.html?_r=1&pagewanted=all&oref=slogin|publisher=nytimes.com|accessdate=2008-03-25}}</ref> In [[2007]] the [[China|Chinese]] military shot down an ageing weather satellite,<ref name="asat"/> followed by the [[US Navy]] shooting down a [[NRO L-21|defunct spy satellite]] in [[February 2008]].<ref>{{citeweb|title=Navy Missile Successful as Spy Satellite Is Shot Down |url=http://www.popularmechanics.com/blogs/science_news/4251430.html|publisher=popularmechanics.com|accessdate=2008-03-25}}</ref>
 +
[[Russia]] and the [[United States]] have also shot down satellites during the [[Cold war]].
 +
 
 +
===Jamming===
 +
Due to the low received signal strength of satellite transmissions they are prone to [[Radio jamming]] by land-based transmitters. Such jamming is limited to the geographical area within the transmitter's range. GPS satellites are potential targets for jamming,<ref>{{citeweb|title=U.S.-Led Forces Destroy GPS Jamming Systems in Iraq |url=http://www.space.com/news/gps_iraq_030325.html|publisher=space.com|accessdate=2008-03-25}}</ref><ref>{{citeweb|title=Homemade GPS jammers raise concerns|url=http://www.computerworld.com/securitytopics/security/story/0,10801,77702,00.html|publisher=computerworld.com|accessdate=2008-03-25}}</ref> but satellite phone and television signals have also been subjected to jamming.<ref>{{citeweb|title=Iran government jamming exile satellite TV|url=http://www.iranfocus.com/modules/news/article.php?storyid=2852|publisher=iranfocus.com|accessdate=2008-03-25}}</ref><ref>{{citeweb|title=Libya Pinpointed as Source of Months-Long Satellite Jamming in 2006|url=http://www.space.com/spacenews/businessmonday_070409.html|publisher=space.com|accessdate=2008-03-25}}</ref>
 +
 
 +
==Satellite Services==
 +
* [[Satellite Internet access]]
 +
* [[Satellite phone]]
 +
* [[Satellite radio]]
 +
* [[Satellite television]]
 +
* [[Satellite navigation]]
  
 
==See also==
 
==See also==
{{Portal | Spaceflight | Spaceship and the Sun.jpg}}
+
{{Portal | Spaceflight | RocketSunIcon.svg}}
[[Image:Satellite.JPG|thumbnail|right|A model satellite in a museum]]
+
 
* [[Communications satellite]]
+
* [[2007 Chinese anti-satellite missile test]]
* [[Timeline of artificial satellites and space probes]]
+
* [[Footprint (satellite)]]
 +
* [[Fractionated Spacecraft]]
 +
* [[GoldenEye (fictional satellite weapon)]]
 +
* [[International Designator]]
 +
* [[IMINT]]
 
* [[List of Earth observation satellites]]
 
* [[List of Earth observation satellites]]
* [[International Designator]]
 
 
* [[Satellite Catalog Number]]
 
* [[Satellite Catalog Number]]
* [[Miniaturized satellite]]
 
 
* [[Satellite formation flying]]
 
* [[Satellite formation flying]]
* Satellites (sorted by launch date):
+
* [[Smallsat]]
** [[Syncom]] 1 (1963), 2 (1963) and 3 (1964)
+
* [[Space debris]]
** [[Anik 1]] (1972)
+
* [[USA 193]]
** [[EgyptSat 1]] (2007) (Egypt, launched by Ukraine)
 
** [[Aryabhata (satellite)|Aryabhata]] (1975) (India, launched by USSR)
 
** [[Hermes Communications Technology Satellite]] (1976)
 
** [[Experimental geodetic payload]] (1986)
 
** [[Munin (satellite)|Munin]] (2000) (Sweden, launched by U.S.)
 
** [[KEO]] satellite—a space [[time capsule]] (2006)
 
* Satellite Services:
 
** [[Satellite phone]]
 
** [[Satellite Internet]]
 
** [[Satellite television]]
 
** [[Satellite radio]]
 
* [[Anti-satellite weapon]]
 
* [[GoldenEye (fictional satellite weapon)]]
 
* [[Tether satellite]]
 
  
==Notes==
+
==References==
{{reflist}}
+
{{reflist|2}}
  
 
==External links==
 
==External links==
All links retrieved November 6, 2007.
+
* [http://dels.nas.edu/basc/earthobservations Earth Observations from Space] A collection of satellite-based images and animations from the National Research Council.  
 
+
* [http://science.nasa.gov/RealTime/JTrack/3D/JTrack3D.html J-Track 3D] A 3-dimensional display of all active satellites orbiting planet Earth.
 
* [http://en.satellite.tracks.free.fr Satellite Ground Tracks] Real time satellite's tracks (Full catalog of satellite orbit). {{en icon}} {{de icon}} {{es icon}} {{fr icon}} {{it icon}} {{pt icon}} {{zh icon}}
 
* [http://en.satellite.tracks.free.fr Satellite Ground Tracks] Real time satellite's tracks (Full catalog of satellite orbit). {{en icon}} {{de icon}} {{es icon}} {{fr icon}} {{it icon}} {{pt icon}} {{zh icon}}
 
* [http://www.vega.org.uk/video/programme/12 'Eyes in the Sky' Free video by the Vega Science Trust and the BBC/OU] Satellites and their implications over the last 50 years.
 
* [http://www.vega.org.uk/video/programme/12 'Eyes in the Sky' Free video by the Vega Science Trust and the BBC/OU] Satellites and their implications over the last 50 years.
 
* [http://science.howstuffworks.com/satellite.htm How Stuff Works.com]  How satellites work
 
* [http://science.howstuffworks.com/satellite.htm How Stuff Works.com]  How satellites work
 
*[http://www.ucsusa.org/global_security/space_weapons/satellite_database.html UCS Satellite Database] Lists operational satellites currently in orbit around the Earth. Updated quarterly.
 
*[http://www.ucsusa.org/global_security/space_weapons/satellite_database.html UCS Satellite Database] Lists operational satellites currently in orbit around the Earth. Updated quarterly.
* [http://www.lsi.usp.br/~rbianchi/clarke/ACC.ETRelaysFull.html Facsimile of Arthur C. Clarke's 1945 paper on communication satellites]
+
*[http://www.satelliteonthenet.co.uk/launch.html Satellite launch schedule]
* [http://www.oosa.unvienna.org UN Office for Outer Space Affairs] ensures all countries benefit from satellites
+
 
* [http://archives.cbc.ca/IDD-1-75-92/science_technology/satellites/ CBC Digital Archives - Launching the Digital Age: Canadian Satellites]
+
{{Space-based meteorological observation}}
* [http://informationvision.net/default.aspx 'Student Satellite Project'] Student Satellite Project for Pakistani and International Students. This site contains information and documents about satellite projects.
+
 
*[http://www.orbitaldebris.jsc.nasa.gov/ NASA Orbital Debris Program Office]
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[[Category:Satellites| ]]
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[[Category:Unmanned vehicles]]
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[[Category:Remote sensing]]
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[[Category:Meteorological data and networks]]
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[[Category:Russian inventions]]
  
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[[Category:physical sciences]]
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Revision as of 00:22, 3 August 2008

This article is about artificial satellites. For natural satellites, also known as moons, see Natural satellite.
Satellites and Satalite redirect here. For the Canadian reggae band, see Sattalites.
For other uses, see Satellite (disambiguation).


A full size model of the Earth observation satellite ERS 2

In the context of spaceflight, a satellite is an object which has been placed into orbit by human endeavor. Such objects are sometimes called artificial satellites to distinguish them from natural satellites such as the Moon.

History

Early conceptions

The first fictional depiction of a satellite being launched into orbit is a short story by Edward Everett Hale, The Brick Moon. The story was serialized in The Atlantic Monthly, starting in 1869.[1][2] The idea surfaces again in Jules Verne's The Begum's Millions (1879).

In 1903 Konstantin Tsiolkovsky (1857–1935) published Исследование мировых пространств реактивными приборами (The Exploration of Cosmic Space by Means of Reaction Devices), which is the first academic treatise on the use of rocketry to launch spacecraft. He calculated the orbital speed required for a minimal orbit around the Earth at 8 km/s, and that a multi-stage rocket fueled by liquid propellants could be used to achieve this. He proposed the use of liquid hydrogen and liquid oxygen, though other combinations can be used.

In 1928 Herman Potočnik (1892–1929) published his sole book, Das Problem der Befahrung des Weltraums - der Raketen-Motor (The Problem of Space Travel — The Rocket Motor), a plan for a breakthrough into space and a permanent human presence there. He conceived of a space station in detail and calculated its geostationary orbit. He described the use of orbiting spacecraft for detailed peaceful and military observation of the ground and described how the special conditions of space could be useful for scientific experiments. The book described geostationary satellites (first put forward by Tsiolkovsky) and discussed communication between them and the ground using radio, but fell short of the idea of using satellites for mass broadcasting and as telecommunications relays.

In a 1945 Wireless World article the English science fiction writer Arthur C. Clarke (1917-2008) described in detail the possible use of communications satellites for mass communications.[3] Clarke examined the logistics of satellite launch, possible orbits and other aspects of the creation of a network of world-circling satellites, pointing to the benefits of high-speed global communications. He also suggested that three geostationary satellites would provide coverage over the entire planet.

History of artificial satellites

The first artificial satellite was Sputnik 1, launched by the Soviet Union on 4 October 1957, and that started the whole Soviet Sputnik program, with Sergei Korolev as chief designer. This triggered the Space Race between the Soviet Union and the United States.

Sputnik 1 helped to identify the density of high atmospheric layers through measurement of its orbital change and provided data on radio-signal distribution in the ionosphere. Because the satellite's body was filled with pressurized nitrogen, Sputnik 1 also provided the first opportunity for meteoroid detection, as a loss of internal pressure due to meteoroid penetration of the outer surface would have been evident in the temperature data sent back to Earth. The unanticipated announcement of Sputnik 1's success precipitated the Sputnik crisis in the United States and ignited the so-called Space Race within the Cold War.

Sputnik 2 was launched on November 3, 1957 and carried the first living passenger into orbit, a dog named Laika.[4]

In May, 1946, Project RAND had released the Preliminary Design of an Experimental World-Circling Spaceship, which stated, "A satellite vehicle with appropriate instrumentation can be expected to be one of the most potent scientific tools of the Twentieth Century.[5] The United States had been considering launching orbital satellites since 1945 under the Bureau of Aeronautics of the United States Navy. The United States Air Force's Project RAND eventually released the above report, but did not believe that the satellite was a potential military weapon; rather, they considered it to be a tool for science, politics, and propaganda. In 1954, the Secretary of Defense stated, "I know of no American satellite program."[citation needed]

On July 29, 1955, the White House announced that the U.S. intended to launch satellites by the spring of 1958. This became known as Project Vanguard. On July 31, the Soviets announced that they intended to launch a satellite by the fall of 1957.

Following pressure by the American Rocket Society, the National Science Foundation, and the International Geophysical Year, military interest picked up and in early 1955 the Air Force and Navy were working on Project Orbiter, which involved using a Jupiter C rocket to launch a satellite. The project succeeded, and Explorer 1 became the United States' first satellite on January 31, 1958.[6]

The largest artificial satellite currently orbiting the Earth is the International Space Station.

Space Surveillance Network

The United States Space Surveillance Network (SSN) has been tracking space objects since 1957 when the Soviets opened the space age with the launch of Sputnik I. Since then, the SSN has tracked more than 26,000 space objects orbiting Earth. The SSN currently tracks more than 8,000 man-made orbiting objects. The rest have re-entered Earth's turbulent atmosphere and disintegrated, or survived re-entry and impacted the Earth. The space objects now orbiting Earth range from satellites weighing several tons to pieces of spent rocket bodies weighing only 10 pounds. About seven percent of the space objects are operational satellites (i.e. ~560 satellites), the rest are space debris.[7] USSTRATCOM is primarily interested in the active satellites, but also tracks space debris which upon reentry might otherwise be mistaken for incoming missiles. The SSN tracks space objects that are 10 centimeters in diameter (baseball size) or larger.

Non-Military Satellite Services

There are three basic categories of non-military satellite services:[8]

Fixed Satellite Service

Fixed satellite services handle hundreds of billions of voice, data, and video transmission tasks across all countries and continents between certain points on the earth’s surface.

Mobile Satellite Systems

Mobile satellite systems help connect remote regions, vehicles, ships and aircraft to other parts of the world and/or other mobile or stationary communications units, in addition to serving as navigation systems.

Scientific Research Satellite (commercial and noncommercial)

Scientific research satellites provide us with meteorological information, land survey data (e.g., remote sensing), and other different scientific research applications such as earth science, marine science, and atmospheric research.

Types

MILSTAR: A communication satellite
  • Anti-Satellite weapons/"Killer Satellites" are satellites that are armed, designed to take out enemy warheads, satellites, other space assets. They may have particle weapons, energy weapons, kinetic weapons, nuclear and/or conventional missiles and/or a combination of these weapons. In fiction, one has been featured in the movie Maximum Overdrive in which one of these, disguised as a "Weather Satellite" had taken out a UFO with Class IV nuclear weapons and laser cannon.
  • Astronomical satellites are satellites used for observation of distant planets, galaxies, and other outer space objects.
  • Biosatellites are satellites designed to carry living organisms, generally for scientific experimentation.
  • Communications satellites are satellites stationed in space for the purpose of telecommunications. Modern communications satellites typically use geosynchronous orbits, Molniya orbits or Low Earth orbits.
  • Miniaturized satellites are satellites of unusually low weights and small sizes.[9] New classifications are used to categorize these satellites: minisatellite (500–200 kg), microsatellite (below 200 kg), nanosatellite (below 10 kg).
  • Navigational satellites are satellites which use radio time signals transmitted to enable mobile receivers on the ground to determine their exact location. The relatively clear line of sight between the satellites and receivers on the ground, combined with ever-improving electronics, allows satellite navigation systems to measure location to accuracies on the order of a few meters in real time.
  • Reconnaissance satellites are Earth observation satellite or communications satellite deployed for military or intelligence applications. Little is known about the full power of these satellites, as governments who operate them usually keep information pertaining to their reconnaissance satellites classified.
  • Earth observation satellites are satellites intended for non-military uses such as environmental monitoring, meteorology, map making etc. (See especially Earth Observing System.)
  • Space stations are man-made structures that are designed for human beings to live on in outer space. A space station is distinguished from other manned spacecraft by its lack of major propulsion or landing facilities — instead, other vehicles are used as transport to and from the station. Space stations are designed for medium-term living in orbit, for periods of weeks, months, or even years.
  • Tether satellites are satellites which are connected to another satellite by a thin cable called a tether.
  • Weather satellites are primarily used to monitor Earth's weather and climate.[10]

Orbit types

Various earth orbits to scale; cyan represents low earth orbit, yellow represents medium earth orbit, the black dashed line represents geosynchronous orbit, the green dash-dot line the orbit of Global Positioning System (GPS) satellites, and the red dotted line the orbit of the International Space Station (ISS).

The first satellite, Sputnik 1, was put into orbit around Earth and was therefore in geocentric orbit. By far this is the most common type of orbit with approximately 2456 artificial satellites orbiting the Earth. Geocentric orbits may be further classified by their altitude, inclination and eccentricity.

The commonly used altitude classifications are Low Earth Orbit (LEO), Medium Earth Orbit (MEO) and High Earth Orbit (HEO). Low Earth orbit is any orbit below 2000 km, and Medium Earth Orbit is any orbit higher than that but still below the altitude for geosynchronous orbit at 35786 km. High Earth Orbit is any orbit higher than the altitude for geosynchronous orbit.

Centric classifications

  • Galactocentric orbit: An orbit about the center of a galaxy. Earth's sun follows this type of orbit about the galactic center of the Milky Way.
  • Heliocentric orbit: An orbit around the Sun. In our Solar System, all planets, comets, and asteroids are in such orbits, as are many artificial satellites and pieces of space debris. Moons by contrast are not in a heliocentric orbit but rather orbit their parent planet.
  • Geocentric orbit: An orbit around the planet Earth, such as the Moon or artificial satellites. Currently there are approximately 2465 artificial satellites orbiting the Earth.
  • Areocentric orbit: An orbit around the planet Mars, such as moons or artificial satellites.

Altitude classifications

  • Low Earth Orbit (LEO): Geocentric orbits ranging in altitude from 0–2000 km (0–1240 miles)
  • Medium Earth Orbit (MEO): Geocentric orbits ranging in altitude from 2000 km (1240 miles) to just below geosynchronous orbit at 35786 km (22240 miles). Also known as an intermediate circular orbit.
  • High Earth Orbit (HEO): Geocentric orbits above the altitude of geosynchronous orbit 35786 km (22240 miles).
Orbital Altitudes of several significant satellites of earth.

Inclination classifications

  • Inclined orbit: An orbit whose inclination in reference to the equatorial plane is not zero degrees.
    • Polar orbit: An orbit that passes above or nearly above both poles of the planet on each revolution. Therefore it has an inclination of (or very close to) 90 degrees.
    • Polar sun synchronous orbit: A nearly polar orbit that passes the equator at the same local time on every pass. Useful for image taking satellites because shadows will be nearly the same on every pass.

Eccentricity classifications

  • Circular orbit: An orbit that has an eccentricity of 0 and whose path traces a circle.
    • Hohmann transfer orbit: An orbital maneuver that moves a spacecraft from one circular orbit to another using two engine impulses. This maneuver was named after Walter Hohmann.
  • Elliptic orbit: An orbit with an eccentricity greater than 0 and less than 1 whose orbit traces the path of an ellipse.
    • Geosynchronous transfer orbit: An elliptic orbit where the perigee is at the altitude of a Low Earth Orbit (LEO) and the apogee at the altitude of a geosynchronous orbit.
    • Geostationary transfer orbit: An elliptic orbit where the perigee is at the altitude of a Low Earth Orbit (LEO) and the apogee at the altitude of a geostationary orbit.
    • Molniya orbit: A highly elliptic orbit with inclination of 63.4° and orbital period of half of a sidereal day (roughly 12 hours). Such a satellite spends most of its time over a designated area of the planet.
    • Tundra orbit: A highly elliptic orbit with inclination of 63.4° and orbital period of one sidereal day (roughly 24 hours). Such a satellite spends most of its time over a designated area of the planet.
  • Hyperbolic orbit: An orbit with the eccentricity greater than 1. Such an orbit also has a velocity in excess of the escape velocity and as such, will escape the gravitational pull of the planet and continue to travel infinitely.
  • Parabolic orbit: An orbit with the eccentricity equal to 1. Such an orbit also has a velocity equal to the escape velocity and therefore will escape the gravitational pull of the planet and travel until its velocity relative to the planet is 0. If the speed of such an orbit is increased it will become a hyperbolic orbit.
    • Escape orbit (EO): A high-speed parabolic orbit where the object has escape velocity and is moving away from the planet.
    • Capture orbit: A high-speed parabolic orbit where the object has escape velocity and is moving toward the planet.

Synchronous classifications

  • Synchronous orbit: An orbit where the satellite has an orbital period equal to the average rotational period (earth's is: 23 hours, 56 minutes, 4.091 seconds) of the body being orbited and in the same direction of rotation as that body. To a ground observer such a satellite would trace an analemma (figure 8) in the sky.
  • Semi-synchronous orbit (SSO): An orbit with an altitude of approximately 20200 km (12544.2 miles) and an orbital period equal to one-half of the average rotational period (earth's is approximately 12 hours) of the body being orbited
  • Geosynchronous orbit (GEO): Orbits with an altitude of approximately 35786 km (22240 miles). Such a satellite would trace an analemma (figure 8) in the sky.
    • Geostationary orbit (GSO): A geosynchronous orbit with an inclination of zero. To an observer on the ground this satellite would appear as a fixed point in the sky.[11]
      • Clarke orbit: Another name for a geostationary orbit. Named after scientist and writer Arthur C. Clarke.
    • Supersynchronous orbit: A disposal / storage orbit above GSO/GEO. Satellites will drift west. Also a synonym for Disposal orbit.
    • Subsynchronous orbit: A drift orbit close to but below GSO/GEO. Satellites will drift east.
    • Graveyard orbit: An orbit a few hundred kilometers above geosynchronous that satellites are moved into at the end of their operation.
      • Disposal orbit: A synonym for graveyard orbit.
      • Junk orbit: A synonym for graveyard orbit.
  • Areosynchronous orbit: A synchronous orbit around the planet Mars with an orbital period equal in length to Mars' sidereal day, 24,6229 hours.
  • Areostationary orbit (ASO): A circular areosynchronous orbit on the equatorial plane and about 17000 km(10557 miles) above the surface. To an observer on the ground this satellite would appear as a fixed point in the sky.
  • Heliosynchronous orbit: An heliocentric orbit about the Sun where the satellite's orbital period matches the Sun's period of rotation. These orbits occur at a radius of 24,360 Gm (0,1628 AU) around the Sun, a little less than half of the orbital radius of Mercury.

Special classifications

  • Sun-synchronous orbit: An orbit which combines altitude and inclination in such a way that the satellite passes over any given point of the planets's surface at the same local solar time. Such an orbit can place a satellite in constant sunlight and is useful for imaging, spy, and weather satellites.
  • Moon orbit: The orbital characteristics of earth's moon. Average altitude of 384403 kilometres (238857 mi), elliptical-inclined orbit.

Pseudo-orbit classifications

  • Horseshoe orbit: An orbit that appears to a ground observer to be orbiting a certain planet but is actually in co-orbit with the planet. See asteroids 3753 (Cruithne) and 2002 AA29.
  • Exo-orbit: A maneuver where a spacecraft approaches the height of orbit but lacks the velocity to sustain it.
    • Suborbital spaceflight: A synonym for exo-orbit.
  • Lunar transfer orbit (LTO)
  • Prograde orbit: An orbit with an inclination of less than 90°. Or rather, an orbit that is in the same direction as the rotation of the primary.
  • Retrograde orbit: An orbit with an inclination of more than 90°. Or rather, an orbit counter to the direction of rotation of the planet. Apart from those in sun-synchronous orbit, few satellites are launched into retrograde orbit because the quantity of fuel required to launch them is much greater than for a prograde orbit. This is because when the rocket starts out on the ground, it already has an eastward component of velocity equal to the rotational velocity of the planet at its launch latitude.
  • Halo orbit and Lissajous orbit: Orbits "around" Lagrangian points.

Satellite Modules

The satellite’s functional versatility is imbedded within its technical components and its operations characteristics. Looking at the “anatomy” of a typical satellite, one discovers two modules.[8] Note that some novel architectural concepts such as Fractionated Spacecraft somewhat upset this taxonomy.

Spacecraft bus or service module

This first module consist of five subsystems:

  • The Structural Subsystems

The structural subsystem provides the mechanical base structure, shields the satellite from extreme temperature changes and micro-meteorite damage, and controls the satellite’s spin functions.

  • The Telemetry Subsystems

The telemetry subsystem monitors the on-board equipment operations, transmits equipment operation data to the earth control station, and receives the earth control station’s commands to perform equipment operation adjustments.

  • The Power Subsystems

The power subsystem consists of solar panels and backup batteries that generate power when the satellite passes into the earth’s shadow.

  • The Thermal Control Subsystems

The thermal control subsystem helps protect electronic equipment from extreme temperatures due to intense sunlight or the lack of sun exposure on different sides of the satellite’s body

  • The Attitude and Orbit Controlled Control Subsystems

The attitude and orbit controlled subsystem consists of small rocket thrusters that keep the satellite in the correct orbital position and keep antennas positioning in the right directions.

Communication Payload

The second major module is the communication payload, which is made up of transponders. A transponders is capable of :

  • Receiving uplinked radio signals from earth satellite transmission stations (antennas).
  • Amplifying received radio signals
  • Sorting the input signals and directing the output signals through input/output signal multiplexers to the proper downlink antennas for retransmission to earth satellite receiving stations (antennas).

Launch-capable countries

Launch of the first British Skynet military satellite.

This list includes countries with an independent capability to place satellites in orbit, including production of the necessary launch vehicle. Note: many more countries have the capability to design and build satellites — which relatively speaking, does not require much economic, scientific and industrial capacity — but are unable to launch them, instead relying on foreign launch services. This list does not consider those numerous countries, but only lists those capable of launching satellites indigenously, and the date this capability was first demonstrated. Does not include consortium satellites or multi-national satellites.

First launch by country
Country Year of first launch First satellite
Flag of Soviet Union Soviet Union 1957 Sputnik 1
Flag of United States United States 1958 Explorer 1
Flag of France France 1965 Astérix
Flag of Japan Japan 1970 Osumi
Flag of People's Republic of China China 1970 Dong Fang Hong I
Flag of United Kingdom United Kingdom 1971 Prospero X-3
Flag of India India 1980 Rohini
Flag of Israel Israel 1988 Ofeq 1

Both North Korea (1998) and Iraq (1989) have claimed orbital launches (satellite and warhead accordingly), but these claims are unconfirmed.

In addition to the above, countries such as South Africa, Spain, Italy, West Germany, Canada, Australia, Argentina, Egypt and private companies such as OTRAG, have developed their own launchers, but have not had a successful launch.

As of 2008, only seven countries from list above ( Russia and Ukraine instead of USSR, also USA, Japan, China, India, and Israel) and one regional organization (the European Space Agency, ESA) have independently launched satellites on their own indigenously developed launch vehicles. (The launch capabilities of the United Kingdom and France now fall under the ESA.)

Several other countries, including South Korea, Iran, Brazil, Pakistan, Romania, Kazakhstan, Australia, Malaysia[citation needed] and Turkey, are at various stages of development of their own small-scale launcher capabilities, and seek membership in the club of space powers.

It is scheduled that in early 2008 South Korea will launch a KSLV rocket (created with assistance of Russia) and become the next space power. Iran already has successfully tested its own space launch vehicle (Kavoshgar 1) and is scheduled to put its first domestic satellite (Omid 1) into orbit within a year from February 4 2008. It is expected that Brazil and Pakistan will follow in the near future..[citation needed]

First launch by country including help of other parties[12]
Country Year of first launch First satellite Payloads in orbit in 2008[13]
Flag of Soviet Union Soviet Union 1957 Sputnik 1 1398
Flag of United States United States 1958 Explorer 1 1042
Flag of Canada Canada 1962 Alouette 1 25
Flag of Italy Italy 1964 San Marco 1 14
Flag of France France 1965 Astérix 44
Flag of Australia Australia 1967 WRESAT 11
Flag of Germany Germany 1969 Azur 27
Flag of Japan Japan 1970 Osumi 111
Flag of People's Republic of China China 1970 Dong Fang Hong I 64
Flag of United Kingdom United Kingdom 1971 Prospero X-3 25
Flag of Poland Poland 1973 Intercosmos Kopernikus 500 ?
Flag of Netherlands Netherlands 1974 ANS 5
Flag of Spain Spain 1974 Intasat 9
Flag of India India 1975 Aryabhata 34
Flag of Indonesia Indonesia 1976 Palapa A1 10
Flag of Czechoslovakia Czechoslovakia 1978 Magion 1 5
Flag of Bulgaria Bulgaria 1981 Intercosmos 22
Flag of Brazil Brazil 1985 Brasilsat A1 11
Flag of Mexico Mexico 1985 Morelos 1 7
Flag of Sweden Sweden 1986 Viking 11
Flag of Israel Israel 1988 Ofeq 1 7
Flag of Luxembourg Luxembourg 1988 Astra 1A 15
Flag of Argentina Argentina 1990 Lusat 10
Flag of Pakistan Pakistan 1990 Badr-1 5
Flag of South Korea South Korea 1992 Kitsat A 10
Flag of Portugal Portugal 1993 PoSAT-1 1
Flag of Thailand Thailand 1993 Thaicom 1 6
Flag of Turkey Turkey 1994 Turksat 1B 5
Flag of Chile Chile 1995 FASat-Alfa 1
Flag of Malaysia Malaysia 1996 MEASAT 4
Flag of Norway Norway 1997 Thor 2 3
Flag of Philippines Philippines 1997 Mabuhay 1 2
Flag of Egypt Egypt 1998 Nilesat 101 3
Flag of Denmark Denmark 1999 Ørsted 3
Flag of South Africa South Africa 1999 SUNSAT 1
Flag of Saudi Arabia Saudi Arabia 2000 Saudisat 1A 12
Flag of United Arab Emirates United Arab Emirates 2000 Thuraya 1 3
Flag of Algeria Algeria 2002 Alsat 1 1
Flag of Greece Greece 2003 Hellas Sat 2 2
Flag of Nigeria Nigeria 2003 Nigeriasat 1 2
Flag of Iran Iran 2005 Sina-1 1
Flag of Kazakhstan Kazakhstan 2006 KazSat 1 1
Flag of Colombia Colombia 2007 Libertad 1 1
Flag of Vietnam Vietnam 2008 VINASAT-1 1

While Canada was the third country to build a satellite which was launched into space,[14] it was launched aboard a U.S. rocket from a U.S. spaceport. The same goes for Australia, who launched on-board a donated Redstone rocket. The first Italian-launched was San Marco 1, launched on 15 December, 1964 on a U.S. Scout rocket from Wallops Island (VA,USA) with an Italian Launch Team trained by NASA.[15] Australia's launch project, in November 1967, involved a donated U.S. missile and U. S. support staff as well as a joint launch facility with the United Kingdom.[16] Kazakhstan claimed to have made their satellite independently[citation needed], but the satellite was built with Russian help, like Polish and Bulgarian ones earlier.

Attacks on satellites

In recent times satellites have been hacked by militant organisations to broadcast propaganda and to pilfer classified information from military communication networks.[17][18]

Satellites in low earth orbit have been destroyed by ballistic missiles launched from earth. Both Russia and the United States have demonstrated ability to eliminate satellites.[19] In 2007 the Chinese military shot down an ageing weather satellite,[19] followed by the US Navy shooting down a defunct spy satellite in February 2008.[20] Russia and the United States have also shot down satellites during the Cold war.

Jamming

Due to the low received signal strength of satellite transmissions they are prone to Radio jamming by land-based transmitters. Such jamming is limited to the geographical area within the transmitter's range. GPS satellites are potential targets for jamming,[21][22] but satellite phone and television signals have also been subjected to jamming.[23][24]

Satellite Services

  • Satellite Internet access
  • Satellite phone
  • Satellite radio
  • Satellite television
  • Satellite navigation

See also

Portal Satellite Portal
  • 2007 Chinese anti-satellite missile test
  • Footprint (satellite)
  • Fractionated Spacecraft
  • GoldenEye (fictional satellite weapon)
  • International Designator
  • IMINT
  • List of Earth observation satellites
  • Satellite Catalog Number
  • Satellite formation flying
  • Smallsat
  • Space debris
  • USA 193

References
ISBN links support NWE through referral fees

  1. The Brick Moon and Other Stories by Edward Everett Hale. Project Gutenberg. Retrieved 2008-03-06.
  2. Contents - The Atlantic monthly. Volume 24, Issue 141. cornell.edu. Retrieved 2008-03-06.
  3. The_1945_Proposal_by_Arthur_C._Clarke_for_Geostationary_Satellite_Communications. lakdiva.org. Retrieved on 2008-03-06.
  4. A Brief History of Animals in Space. NASA. Retrieved 2007-08-08.
  5. Preliminary Design of an Experimental World-Circling Spaceship. RAND. Retrieved on 2008-03-06.
  6. News Reel - First US Satellite Launched. webcastr.com. Retrieved on 2008-03-05.
  7. ORBITAL_DEBRIS_EDUCATION_PACKAGE. nasa.gov. Retrieved on 2008-03-06.
  8. 8.0 8.1 Grant, A.,& Meadows, J. (2004). Satellites Communication. Communication Technology Update (ninth edition). Burlington: Focal Press.
  9. Workshop on the Use of Microsatellite Technologies. United Nations. Retrieved on 2008-03-06.
  10. Earth_Observations_from_Space_The_First_50_Years_of_Scientific_Achievements. nas.edu. Retrieved on 2008-03-06.
  11. PEARL HARBOR IN SPACE. jamesoberg.com. Retrieved on 2008-03-06.
  12. First time in History. tbs-satellite.com. Retrieved on 2008-03-06.
  13. SATCAT Boxscore. celestrak.com. Retrieved on 2008-03-05.
  14. Canada's Churchill Spaceport. spacetoday.org. Retrieved on 2008-03-06.
  15. San Marco 1. nasa.gov. Retrieved on 2008-03-05.
  16. WRESAT_Australia's_First_Satellite. powerup.com.au. Retrieved on 2008-03-05.
  17. Hack a Satellite while it is in orbit. ittoolbox.com. Retrieved on 2008-03-25.
  18. AsiaSat accuses Falungong of hacking satellite signals. Press Trust of India. Retrieved on 2008-03-25.
  19. 19.0 19.1 China Tests Anti-Satellite Weapon, Unnerving U.S.. nytimes.com. Retrieved on 2008-03-25.
  20. Navy Missile Successful as Spy Satellite Is Shot Down. popularmechanics.com. Retrieved on 2008-03-25.
  21. U.S.-Led Forces Destroy GPS Jamming Systems in Iraq. space.com. Retrieved on 2008-03-25.
  22. Homemade GPS jammers raise concerns. computerworld.com. Retrieved on 2008-03-25.
  23. Iran government jamming exile satellite TV. iranfocus.com. Retrieved on 2008-03-25.
  24. Libya Pinpointed as Source of Months-Long Satellite Jamming in 2006. space.com. Retrieved on 2008-03-25.

External links


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