Physics, asked by vpnffshoaib, 6 hours ago

Calculate period of revolution of a polar satellite
orbiting close to the surface of the earth.
(R=6400 km, g = 9.8 m/s2)

Answers

Answered by AnshikaDhiman100

3

Answer:

Given: Radius of earth = R = 6400 km = 6.4 x 106 m, Time period = T = 27.3 days = 27.3 x 24 x 60 x 60, g = 9.8 m/

Explanation:

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