An earth’s satellite of mass m revolves in a circular orbit at a height h from the surface g is acceleration due to gravity at the surface of the earth. The velocity of the satellite in the orbit is given by?
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Velocity of the satellite is underoot 2gr
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it is nothing but orbital velocity i.e, v=√gr
where g is the acceleration due to gravity, r is the radius of earth...
where g is the acceleration due to gravity, r is the radius of earth...
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