Physics, asked by vpnffshoaib, 2 months ago

Calculate period of revolution of a polar satellite
orbiting close to the surface of the earth.
(R = 6400 km, g = 9.8 m/s)

Answers

Answered by utkarshkhandelwal427

1

Answer:

divide it by Rto g

u will get ans 980 this

hope it helps you

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