Geosynchronous orbit
A
geosynchronous orbit is a geocentric
orbit that has the same
orbital period as the
sidereal rotation period of the
Earth. It has a
semi-major axis of 42,164 km (26,200 miles). In the special case of the
geostationary orbit, an observer on the ground would not perceive the satellite as moving and would see it as a fixed point in the sky. Such orbits are useful for
telecommunications relays. In the more general case, when the orbit has some
inclination and/or
eccentricity, the satellite would appear to describe a more or less distorted figure-eight in the sky, and would rest above the same spots of the Earth's surface once per sidereal day.
Synchronous orbits exist around all moons, planets, stars and black holes —unless they rotate so slowly that the orbit would be outside their
Hill sphere. Most inner moons of planets have
synchronous rotation, so their synchronous orbits are, in practice, limited to their leading and trailing
Lagrange points. Objects with
chaotic rotations (such as
Hyperion) are also problematic, as their synchronous orbits keep changing unpredictably.
If a geosynchronous orbit is circular and equatorial then it is also a
geostationary orbit, and will maintain the same position relative to the Earth's surface. If one could see a satellite in geostationary orbit, it would appear to hover at the same point in the sky, i.e., not exhibit
diurnal motion, while one would see the Sun, Moon, and stars traverse the heavens behind it.
A circular geosynchronous orbit in the plane of the Earth's equator has a radius of approximately 42,164 km (from the centre of the Earth) or approximately
35,786 km (22,236
statute miles) above
mean sea level.
Circular geosynchronous orbits at the
equator are known as geostationary orbits. A perfect stable geostationary orbit is an ideal that can only be approximated. In practice the satellite will drift out of this orbit (because of perturbations such as the
solar wind,
radiation pressure, variations in the Earth's gravitational field, and the
gravitational effect of the
Moon and
Sun), and thrusters are used to maintain the orbit in a process known as
stationkeeping.
See Geostationary orbit.
Elliptical orbits can be and are designed for
communications satellites that keep the satellite within view of its assigned ground stations or receivers. A satellite in an elliptical geosynchronous orbit will appear to oscillate in the sky from the viewpoint of a ground station, tracing an
analemma in the sky. Satellites in highly elliptical orbits must be tracked by steerable
ground stations.
Theoretically an
active geosynchronous orbit can be maintained if forces other than gravity are also used to maintain the orbit, such as a
solar sail. Such a
statite can be geosynchronous in an orbit different (higher, lower, more or less elliptical, or some other path) from the
conic section orbit formed by a gravitational body. Such devices are still theoretical.
A further form of geosynchronous orbit is obtained by the theoretical
space elevator in which one end of the structure is tethered to the ground, maintaining a longer orbital period than by gravity alone if under tension.
Other definitions of geosynchronous orbit
* Geosynchronous orbit (GEO): 35786 km above Earth's surface
The following orbits are special orbits that are also used to categorize orbits:
*
Geostationary orbit (GSO): zero inclination geosynchronous orbit
*
Supersynchronous orbit or drift orbit - orbit above GEO. Satellites will drift in a westerly direction.
** (GEO + 235 km + (1000 × CR × A/m) km)
*** where CR is the solar pressure radiation coefficient (typically between 1.2 and 1.5) and A/m is the aspect area [m
2] to dry mass [kg] ratio
*
Subsynchronous orbit or drift orbit - orbits close to but below GEO. Used for satellites undergoing station changes in an eastern direction.
Author
Arthur C. Clarke is credited with popularizing the notion of using a geostationary orbit for communications satellites. The orbit is also known as the
Clarke Orbit. Together, the collection of artificial satellites in these orbits is known as the
Clarke Belt.
The first communications satellite placed in a geosynchronous orbit was
Syncom 2, launched in
1963. Geosynchronous orbits have been in common use ever since, including satellite
television.
Initially, geostationary satellites also carried
telephone calls but are no longer used so predominantly for voice communication, partly due to the inherent disconcerting delay in getting information to the satellite and back (it takes light or radio about a quarter of a second to make the round trip). Similarly, international
Internet connectivity has shifted away from satellite links.
Nearly all land locations on the planet now have terrestrial communications facilities (
microwave,
fiber-optics), even undersea, with more than sufficient capacity. Satellite telephony is now mainly limited to small, isolated locations that have no terrestrial facilities, such as
Canada's arctic islands,
Antarctica, the far reaches of
Alaska and
Greenland, and ships at sea (via
Inmarsat).
*
Geostationary orbit*
Geosynchronous satellite*
Synchronous rotation*
Geosynchronous network*
Nasa.gov: Geosynchronous Orbit*
Science Presse data on Geosynchronous Orbits (including historical data and launch statistics)*
ORBITAL MECHANICS (Rocket and Space Technology)
