Solution: Here, gravitational force will be equal to centripetal force acting on satellite.
Thus, GMm/R2 = mv2/R
( M- mass of Earth and m is mass of satellite and R is distance between centre of the Earth to satellite = radius of Earth + Height of satellite = 6370+7655 = 14025 km = 1.4025*10^7 m and G is gravitational constant = 6.674 * 10-11 m3 kg-1 s-2)
=> GM/R = v2
=> v = √ (GM/R)
=> v = √ { (6.674 * 10-11) (5.97*1024 )/(1.4025*107)}
=> v = 5330.01 m/s. Answer
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