Difference between revisions of "Satellite" - New World Encyclopedia

From New World Encyclopedia
(imported, credited, and categorized)
 
(article ready, image(s) currently in article are ok to use)
Line 1: Line 1:
 +
{{ready}}{{images OK}}
 +
 
[[Image:ERS 2.jpg|thumb|right|300px|An Earth observation satellite, [[ERS 2]]]]
 
[[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]].
 
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 ==
 
==Early theoretical work on artificial satellites ==
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>
+
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).
{{cite web | url = http://www.gutenberg.org/etext/1633 | title = The Brick Moon and Other Stories by Edward Everett Hale | publisher = Project Gutenberg}}</ref>{{,}}<ref>
 
{{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 University Library}}</ref> 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&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.
+
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.
  
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 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]] (b. 1917) described in detail the possible use of [[communications satellite]]s for mass communications.<ref>facsimile at http://www.lsi.usp.br/~rbianchi/clarke/ACC.ETRelaysFull.html</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.
+
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.
  
 
== History of artificial satellites ==
 
== History of artificial satellites ==
 
{{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]].
+
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]].
  
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>
+
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>
{{cite web | url = http://www.rand.org/pubs/special_memoranda/SM11827/index.html | title = Preliminary Design of an Experimental Worip | publisher = [[RAND]]}}</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."
 
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."
  
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.
+
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]].
+
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.
  
 
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]].
Line 32: Line 31:
  
 
== Non-Military Satellite Services ==
 
== Non-Military Satellite Services ==
There are three basic categories of non-military satellite services: <ref>Grant, A.,& Meadows, J. (2004). Satellites Communication. Communication Technology Update (ninth edition). Burlington: Focal Press.</ref>
+
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>
  
 
=== Fixed Satellite Service ===
 
=== Fixed Satellite Service ===
Line 44: Line 43:
 
==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]]
+
* '''[[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]]
 
*'''[[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.
Line 52: Line 51:
 
*'''[[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]].)
 
*'''[[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]].)
*'''[[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.
+
*'''[[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]].
 
*'''[[Weather satellite]]s''' are satellites that primarily are used to monitor [[Earth]]'s [[weather]] and [[climate]].
  
Line 60: Line 59:
 
===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]].  
 
* '''[[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]].  
* '''[[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.
+
* '''[[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]].
+
* '''[[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 [[mile]]s). Also known as an [[intermediate circular orbit]].
+
* '''[[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]].
 
* '''[[High Earth Orbit]] (HEO)''': [[Geocentric orbit]]s above the altitude of [[geosynchronous orbit]] 35,786 [[km]] (22,240 [[mile]]s).
 
* '''[[High Earth Orbit]] (HEO)''': [[Geocentric orbit]]s above the altitude of [[geosynchronous orbit]] 35,786 [[km]] (22,240 [[mile]]s).
  
Line 78: Line 77:
 
** '''[[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]].
+
** '''[[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]].
+
** '''[[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 100: Line 99:
 
* '''[[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 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.
* '''[[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===
Line 107: Line 106:
  
 
=== 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]].
 
** '''[[Orbital 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]].
  
 
Satellites can also orbit [[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>Grant, A.,& Meadows, J. (2004). Satellites Communication. Communication Technology Update (ninth edition). Burlington: Focal Press.</ref>
+
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"/>
  
 
=== Spacecraft bus or service module ===  
 
=== Spacecraft bus or service module ===  
Line 140: Line 139:
 
==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.
+
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>[http://www.celestrak.com/satcat/boxscore.asp]</ref>
+
! 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>
 
|-
 
|-
|align="left"| {{flag|Soviet Union}}<br>{{flag|Russia}}<br>{{flag|Ukraine}} || 1957 || ''[[Sputnik 1]]'' || 1390
+
|align="left"| {{flag|Soviet Union}}<br/>{{flag|Russia}}<br/>{{flag|Ukraine}} || 1957 || ''[[Sputnik 1]]'' || 1390
 
|-
 
|-
 
|align="left"| {{flag|United States}} || 1958 || ''[[Explorer 1]]'' || 999
 
|align="left"| {{flag|United States}} || 1958 || ''[[Explorer 1]]'' || 999
Line 171: Line 170:
 
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.
 
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]].)
+
[[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]].)
  
 
Also, one international private company ([[Sea Launch]]) has launch capability through their purchase of Ukrainian–Russian launchers.
 
Also, one international private company ([[Sea Launch]]) has launch capability through their purchase of Ukrainian–Russian launchers.
Line 182: Line 181:
 
|+ '''First launch by country including help of other parties'''
 
|+ '''First launch by country including help of other parties'''
 
|- bgcolor=#efefef
 
|- bgcolor=#efefef
! Country || Year of first launch || First satellite || Payloads in orbit in 2006<ref>[http://www.celestrak.com/satcat/boxscore.asp]</ref>
+
! Country || Year of first launch || First satellite || Payloads in orbit in 2006<ref name="boxscore"/>
 
|-
 
|-
|align="left"| {{flag|Soviet Union}}<br>{{flag|Russia}}<br>{{flag|Ukraine}} || 1957 || ''[[Sputnik 1]]'' || 1390
+
|align="left"| {{flag|Soviet Union}}<br/>{{flag|Russia}}<br/>{{flag|Ukraine}} || 1957 || ''[[Sputnik 1]]'' || 1390
 
|-
 
|-
 
|align="left"| {{flag|United States}} || 1958 || ''[[Explorer 1]]'' || 999
 
|align="left"| {{flag|United States}} || 1958 || ''[[Explorer 1]]'' || 999
Line 215: Line 214:
 
|}
 
|}
  
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]</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]</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, 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.
  
 
==Heraldry==
 
==Heraldry==
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], Heraldry.ca</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]].
+
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]].
  
 
==See also==
 
==See also==
Line 238: Line 237:
 
** [[Experimental geodetic payload]] (1986)
 
** [[Experimental geodetic payload]] (1986)
 
** [[Munin (satellite)|Munin]] (2000) (Sweden, launched by U.S.)
 
** [[Munin (satellite)|Munin]] (2000) (Sweden, launched by U.S.)
** [[KEO]] satellite — a space [[time capsule]] (2006)
+
** [[KEO]] satellite—a space [[time capsule]] (2006)
 
* Satellite Services:
 
* Satellite Services:
 
** [[Satellite phone]]
 
** [[Satellite phone]]
Line 248: Line 247:
 
* [[Tether satellite]]
 
* [[Tether satellite]]
  
==References==
+
==Notes==
 
{{reflist}}
 
{{reflist}}
  
 
==External links==
 
==External links==
 +
All links retrieved November 6, 2007.
 +
 
* [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.edusat.info Edusat project]
 
 
* [http://www.lsi.usp.br/~rbianchi/clarke/ACC.ETRelaysFull.html Facsimile of Arthur C. Clarke's 1945 paper on communication satellites]
 
* [http://www.lsi.usp.br/~rbianchi/clarke/ACC.ETRelaysFull.html Facsimile of Arthur C. Clarke's 1945 paper on communication satellites]
 
* [http://www.oosa.unvienna.org UN Office for Outer Space Affairs] ensures all countries benefit from satellites
 
* [http://www.oosa.unvienna.org UN Office for Outer Space Affairs] ensures all countries benefit from satellites

Revision as of 15:23, 6 November 2007


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 satellites such as the Moon.

Early theoretical work on artificial satellites

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.[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/second, 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. 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.

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 (b. 1917) 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. This triggered the Space Race between the Soviet Union and the United States.

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.[4] 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."

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.

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. 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: [5]

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

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, 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 USSR Tests ASAT weapon and ASAT Test. See also IMINT
  • 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. 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.
  • Weather satellites are satellites that primarily are used to monitor Earth's weather and climate.

Orbit types

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.
  • 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 (1,240 miles) to just below geosynchronous orbit at 35,786 km (22,240 miles). Also known as an intermediate circular orbit.
  • High Earth Orbit (HEO): Geocentric orbits above the altitude of geosynchronous orbit 35,786 km (22,240 miles).

Inclination classifications

  • Inclined orbit: An orbit whose inclination in reference to the equatorial plane is not 0.
    • 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 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 20,200 km (12544.2 miles) and an orbital period of approximately 12 hours
  • 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.
    • 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.
      • Clarke orbit: Another name for a geostationary orbit. Named after the 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 17,000 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 384,403 kilometres (238,857 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.
    • Orbital 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.

Satellites can also orbit 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 satellite, one discover two modules. [5]

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 is comprised of solar panel 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 Altitude 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.

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

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 Launches to orbit in 2006[6]
Flag of Soviet Union Soviet Union
Flag of Russia Russia
Flag of Ukraine Ukraine
1957 Sputnik 1 1390
Flag of United States United States 1958 Explorer 1 999
Flag of France France 1965 Astérix 43
Flag of Australia Australia 1967 WRESAT 1
Flag of Japan Japan 1970 Osumi 102
Flag of People's Republic of China China 1970 Dong Fang Hong I 53
Flag of United Kingdom United Kingdom 1971 Prospero X-3 23[citation needed]
Flag of India India 1981 Rohini 31
Flag of Israel Israel 1988 Ofeq 1 6

Both North Korea (1998) and Iraq (1989) have claimed orbital launches, 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.)

Also, one international private company (Sea Launch) has launch capability through their purchase of Ukrainian–Russian launchers.

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.

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.

First launch by country including help of other parties
Country Year of first launch First satellite Payloads in orbit in 2006[6]
Flag of Soviet Union Soviet Union
Flag of Russia Russia
Flag of Ukraine Ukraine
1957 Sputnik 1 1390
Flag of United States United States 1958 Explorer 1 999
Flag of Canada Canada 1962 Alouette 1 33
Flag of Italy Italy 1964 San Marco 1
Flag of France France 1965 Astérix 43
Flag of Australia Australia 1967 WRESAT
Flag of Japan Japan 1970 Osumi 102
Flag of People's Republic of China China 1970 Dong Fang Hong I 53
Flag of United Kingdom United Kingdom 1971 Prospero X-3 23
Flag of India India 1975 Aryabhata 31
Flag of Israel Israel 1988 Ofeq 1 6
Flag of Portugal Portugal 1993 PoSAT-1
Flag of Egypt Egypt 1998 NileSat 101 3
Flag of Iran Iran 2005 Sina-1 1
Flag of Kazakhstan Kazakhstan 2006 KazSat 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.[7]. 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.[8] Kazakhstan claimed to have launched their satellite independently, but the satellite was built with Russian help.

Heraldry

The (artificial, though this is not stated in the blazon) satellite appears as a charge in the arms of Arthur Maxwell House.[9] This is in addition to numerous appearances of the natural satellite the moon, and the moons of the planets Jupiter and Saturn (with those planets) in the arms of Pierre-Simon LaPlace.

See also

Portal Satellite Portal
File:Satellite.JPG
A model satellite in a museum
  • Communications satellite
  • Timeline of artificial satellites and space probes
  • List of Earth observation satellites
  • International Designator
  • Satellite Catalog Number
  • Miniaturized satellite
  • Satellite formation flying
  • Satellites (sorted by launch date):
    • Syncom 1 (1963), 2 (1963) and 3 (1964)
    • Anik 1 (1972)
    • EgyptSat 1 (2007) (Egypt, launched by Ukraine)
    • Aryabhata (1975) (India, launched by USSR)
    • Hermes Communications Technology Satellite (1976)
    • Experimental geodetic payload (1986)
    • 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

  1. The Brick Moon and Other Stories by Edward Everett Hale - Retrieved November 6, 2007.
  2. Contents - The Atlantic monthly. Volume 24, Issue 141 - Retrieved November 6, 2007.
  3. Arthur C. Clarke Extra Terrestrial Relays - Retrieved November 6, 2007.
  4. Preliminary Design of an Experimental Worip - Retrieved November 6, 2007.
  5. 5.0 5.1 August E Grant, and Jennifer Harman Meadows. Communication Technology Update (ninth edition). (Burlington: Focal Press, 2004, ISBN 9780080470320)
  6. 6.0 6.1 CelesTrak WWW: SATCAT Boxscore - Retrieved November 6, 2007.
  7. NSSDC Master Catalog Display: Spacecraft - Retrieved November 6, 2007.
  8. WRESAT - Retrieved November 6, 2007.
  9. Arms of the House family - Retrieved November 6, 2007.

External links

All links retrieved November 6, 2007.

Credits

New World Encyclopedia writers and editors rewrote and completed the Wikipedia article in accordance with New World Encyclopedia standards. This article abides by terms of the Creative Commons CC-by-sa 3.0 License (CC-by-sa), which may be used and disseminated with proper attribution. Credit is due under the terms of this license that can reference both the New World Encyclopedia contributors and the selfless volunteer contributors of the Wikimedia Foundation. To cite this article click here for a list of acceptable citing formats.The history of earlier contributions by wikipedians is accessible to researchers here:

The history of this article since it was imported to New World Encyclopedia:

Note: Some restrictions may apply to use of individual images which are separately licensed.