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[" The work done to increase the radius of orbit "],[" of a satellite of mass 'm' revolving around a "],[" planet of mass M from orbit of radius "R" in to "],[" another orbit of radius "3R" is "],[" 1) "(2GMm)/(3R)" 2) "(GMm)/(3R)" 3) "(GMm)/(6R)" 4) "(GMm)/(24R)]

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