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at a particular point in orbit a satellite in an elliptical orbit has a gravitational PE of 6000 MJ with respect to earth's surface and
at a particular point in orbit a satellite in an elliptical orbit has a gravitational PE of 6000 MJ with respect to earth's surface and a KE of 5000 MJ. later in its orbit, the satellite's PE is 7000 MJ. what is its KE at that point? explain
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