The orbital velocity of an artificial satellite in a circular orbit just above the centre's surface is v. For a satellite orbiting at an altitude of half of the earth's radius, the orbital velocity is :
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Vo is the Orbital Velocity. Vo = Root gR
Chakshu290703:
isnt it root GM/R
but the options consist of a)3v/2 b)root over 3/2v. c)root over2/3v. c)(2/3)v
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