Geography, asked by RUPANKAJ7979, 10 months ago

95 geostationary orbit is at a height of

a. 6km

b. 1000km

c. 3600km

d. 36000km

Answers

Answered by priyanshu2882003

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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