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geostationary orbit
(redirected from GEO orbit)

   Also found in: Wikipedia 0.06 sec.

geostationary orbit

Circular path 35,900 km/22,300 mi above the Earth's Equator on which a satellite takes 24 hours, moving from west to east, to complete an orbit, thus appearing to hang stationary over one place on the Earth's surface. Geostationary orbits are used particularly for communications satellites and weather satellites. Their use for communications satellites was first suggested by the English space writer Arthur C Clarke. A geosynchronous orbit lies at the same distance from Earth but is inclined to the Equator.



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It has payload power requirements in the range of 2500 W to 5000 W, and one of the satellites will be configured with a Li-ion Battery to provide 100% payload power support during eclipses and with a design life of 15 years in GEO orbit.
 
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