If r represents the radius of the orbit of a satellite of mass m moving around a planet of mass M,the velocity of the satellite is given by: a)v^2 = gM/r b)v^2 = GMm/r c)v = GM/r d)v^2 = GM/r
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here is the answer is option d
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mdtushaara:
Thank you bro.......
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Option d is the correct answer.
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