Question

What is the period revolution of geostationary satellite?

Answer 1

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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 onesidereal day (23.934461223 hours).

Answer 2

23.934461223 hours
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