What is the kinetic energy of a satellite of mass m in that orbits the Earth, of mass M, in a circular orbit of radius R?
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Answer: However the total energy INPUT required to put a satellite into an orbit of radius r around a planet of mass M and radius R is therefore the sum of the gravitational potential energy (GMm[1/R-1/r]) and the kinetic energy of the satellite (VxGMm/r).
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