what do you know about height and velocity of geostationary satellite
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A geostationary orbit can be achieved only at an altitude very close to 35,786 km (22,236 mi) and directly above the equator. This equates to an orbital velocity of 3.07 km/s (1.91 mi/s) and an orbital period of 1,436 minutes, which equates to almost exactly one sidereal day (23.934461223 hours).
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It's height is 36750 km or more...
It's velocity is similar to velocity of earth's rotation around itself...
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