A satellite of earth of mass m taken from orbital radius 2r to 3r
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✔Energy required = (Potential energy of the Earth – mass system when mass is at distance 3R) – (Potential energy of the Earth-mass system when mass is at distance 2R)
= - GM/3R – (-GM/2R) = - GM/3R + GM/2R
= -2GMm+3GMm / 6R = GMm/6R
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