why is the energy for satellite GMm/2R
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The kinetic energy of an object in orbit can easily be found from the following equations:
Centripetal force on a satellite of mass m moving at velocity v in an orbit of radius r = mv2/r
But this is equal to the gravitational force (F) between the planet (mass M) and the satellite:
F =GMm/r2 and so mv2 = GMm/r
But kinetic energy = ½mv2 and so:
kinetic energy of the satellite = ½ GMm/r
Explanation:
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