Question

what is period of revolution of a satellite.? ​

Answer 1

Hi friend here is your answer.

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T=(2×pi)×root(r^3/Gm)

T=time period

r=radius and G=Gravitational constant

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Answer 2

it's is given by the relation ,,,

2πr/ speed(tangential velocity)

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it depends on the height of the satellite also.