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[" If "^(6)V(e)" ' is the escape velocit...

[" If "^(6)V_(e)" ' is the escape velocity of a body from a "],[" planet of mass "^(6)M" ' and radius "^(6)R" '.Then the "],[" velocity of the satellite revolving at height "^(6)h" ' "],[" from the surface of the planet will be "],[v_(e)sqrt((R)/(R+h))" 2) "v_(e)sqrt((2R)/(R+h))" 3) "v_(e)sqrt((R+h)/(R))" 4) "v_(e)sqrt((R)/(2(R+h)))]

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