Question

what do you know about height and velocity of geostationary satellite

Answer 1

Answer:

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).

Answer 2

Answer:

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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