- List of orbits
The following is a list of types of orbits:
Centric classifications
* Galactocentric orbit: An orbit about the center of a
galaxy .Earth 'ssun follows this type of orbit about thegalactic center of theMilky Way .
*Heliocentric orbit : Anorbit around theSun . In ourSolar System , allplanets ,comets , andasteroids are in such orbits, as are many artificial satellites and pieces ofspace debris . Moons by contrast are not in aheliocentric orbit but rather orbit their parent planet.
*Geocentric orbit : An orbit around the planetEarth , such as theMoon orartificial satellite s. Currently there are approximately 2,465 artificial satellites orbiting theEarth .
*Areocentric orbit : An orbit around the planetMars , such as moons orartificial satellite s.
*Lunar orbit : An orbit around the Earth'smoon .Altitude classifications
*
Low Earth Orbit (LEO):Geocentric orbit s ranging in altitude from 0–2,000km (0–1,240mile s)
*Medium Earth Orbit (MEO):Geocentric orbit s ranging in altitude from 2,000km (1,240mile s) to just belowgeosynchronous orbit at 35,786km (22,240mile s). Also known as anintermediate circular orbit .
*Geosynchronous orbit : The orbit around Earth exactly matching Earth's sidereal rotation period.
*High Earth Orbit (HEO):Geocentric orbit s above the altitude ofgeosynchronous orbit 35,786km (22,240mile s).Inclination classifications
*
Inclined orbit : An orbit whoseinclination in reference to theequatorial plane is not 0.
**Polar orbit : Anorbit that passes above or nearly above both poles of the planet on each revolution. Therefore it has aninclination of (or very close to) 90 degrees.
** Polarsun synchronous orbit (SSO): A nearlypolar orbit that passes theequator at the same localsolar time on every pass. Useful forimage taking satellites becauseshadow s will be the same on every pass.
*Non-inclined orbit : An orbit whoseinclination is equal to zero with respect to someplane of reference .
** Ecliptical orbit: Anon-inclined orbit with respect to theecliptic .
** Equatorial orbit: Anon-inclined orbit with respect to theequator .
*Near equatorial orbit : An orbit whose inclination with respect to theequatorial plane is nearly zero. This orbit allows for rapid revisit times (for a single orbiting spacecraft) of near equatorial ground sites.Eccentricity classifications
*
Circular orbit : Anorbit that has an eccentricity of 0 and whose path traces acircle .
*Elliptic orbit : Anorbit with an eccentricity greater than 0 and less than 1 whose orbit traces the path of anellipse .
**Geosynchronous transfer orbit : Anelliptic orbit where theperigee is at thealtitude of aLow Earth Orbit (LEO) and theapogee at thealtitude of ageosynchronous orbit .
**Geostationary transfer orbit : Anelliptic orbit where theperigee is at thealtitude of aLow Earth Orbit (LEO) and theapogee at thealtitude of ageostationary orbit .
**Hohmann transfer orbit : An orbital maneuver that moves aspacecraft from onecircular orbit to another using two engineimpulse s. This maneuver was named afterWalter Hohmann .
*Hyperbolic trajectory : Anorbit with the eccentricity greater than 1. Such an orbit also has avelocity in excess of theescape velocity and as such, will escape the gravitational pull of theplanet and continue to travelinfinitely .
*Parabolic orbit : Anorbit with the eccentricity equal to 1. Such an orbit also has avelocity equal to theescape velocity and therefore will escape the gravitational pull of theplanet and travel until itsvelocity relative to theplanet is 0. If the speed of such an orbit is increased it will become ahyperbolic orbit .
**Escape orbit (EO): A high-speedparabolic orbit where the object hasescape velocity and is moving away from theplanet .
**Capture orbit : A high-speedparabolic orbit where the object hasescape velocity and is moving toward theplanet .ynchronous classifications
*
Synchronous orbit : An orbit where the satellite has anorbital period equal to the averagerotational period (earth's is: 23hour s, 56minute s, 4.091second s) of the body being orbited and in the same direction of rotation as that body.
*Geosynchronous orbit (GEO): A nearly circular orbit with an altitude of approximately 35,786 km (22,240 miles). Such a satellite traces ananalemma (figure 8) in the sky, as seen from the ground.
**Geostationary orbit (GSO): A circulargeosynchronous orbit with aninclination of zero. To an observer on the ground this satellite would appear as a fixed point in the sky.
***Clarke orbit : Another name for ageostationary orbit . Named after the writerArthur C. Clarke .
*Tundra orbit : A synchronous but highlyelliptic orbit withinclination of 63.4° andorbital period of onesidereal day (roughly 24 hours). Such a satellite spends most of its time over a designated area of theplanet . The particular inclination keeps the perigee shift small.
*Semi-synchronous orbit : Anorbit with anorbital period of approximately 12 hours. If the orbit is circular, this requires analtitude of approximately 20,200 km (12,544.2 miles).
**Molniya orbit : A semi-synchronous but highlyelliptic orbit withinclination of 63.4° andorbital period of half of asidereal day (roughly 12 hours). Such a satellite spends most of its time over two designated areas of theplanet . The particular inclination keeps the perigee shift small.
*Supersynchronous orbit : A disposal / storage orbit above GSO/GEO. Satellites will drift west. Also asynonym 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 abovegeosynchronous that satellites are moved into at the end of their operation.
**Disposal orbit : Asynonym forgraveyard orbit .
**Junk orbit : Asynonym forgraveyard orbit .
*Areosynchronous orbit : Asynchronous orbit around the planetMars with anorbital period equal in length to Mars'sidereal day , 24.6229hours .
*Areostationary orbit (ASO): Acircular areosynchronous orbit on theequatorial plane and about 17,000km (10,557mile s) above the surface of Mars. To an observer on the ground this satellite would appear as a fixed point in the sky.
*Heliosynchronous orbit : Anheliocentric orbit about theSun where the satellite'sorbital period matches theSun 's period ofrotation . These orbits occur at a radius of 24,360 Gm (0.1628 AU) around theSun , a little less than half of theorbital radius of Mercury.pecial classifications
*
Sun-synchronous orbit : An orbit which combinesaltitude andinclination in such a way that the satellite passes over any given point of theplanets 's surface at the same localsolar time . Such an orbit can place a satellite in constant sunlight and is useful forimaging , spy, andweather satellite s.
*Orbit of the Moon : The orbital characteristics ofEarth 'smoon . Averagealtitude of 384,403 kilometres (238,857 mi), elliptical-inclined orbit .Pseudo-orbit classifications
*
Horseshoe orbit : Anorbit that appears to a ground observer to be orbiting a certainplanet but is actually in co-orbit with theplanet . See asteroids3753 Cruithne and 2002 AA29.
*Exo-orbit : A maneuver where aspacecraft achieves anorbit that is unstable due to atmospheric drag.
*Lunar transfer orbit (LTO)
*Prograde orbit : Anorbit 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 : Anorbit with aninclination of more than 90°. Or rather, an orbit counter to the direction of rotation of the planet. Apart from those insun-synchronous orbit , few satellites are launched intoretrograde orbit because the quantity of fuel required to launch them is much greater than for aprograde orbit . This is because when the rocket starts out on the ground, it already has an eastward component ofvelocity equal to the rotational velocity of the planet at its launchlatitude .Other
*
Box orbit
*Ecliptic orbit
*Osculating orbit
*Parking orbit
*Artificial satellite orbit
*Halo orbit
*Lissajous orbit
*Satellites can also orbitLagrangian point s
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