What will be velocity of a satellite revolving
around the earth at a height h above surface of
earth if radius of earth is R
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Hey mate here is your answer............
Given: height of satellite above the surface of earth = h = 700 km, Radius of earth = R = 6400 km, G = 6.67 x 10-11 N m2/kg2 ; g = 9.8 m/s2.
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