A satellite is launched in a circular orbit around Earth of radius R. Time taken by it to complete one
revolution is 20 hours. Find the time period of revolution of a satellite orbiting in a radius of 4R.
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T= 2√(R + h)'3/ GM
T1= 2π√R'3/GM, T2= 2π√(1.01R)'3/GM
T2 - T1/T1 multiply 100 = 1.5%
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