A satellite at a particular point along an elliptical orbit has a gravitational potential energy of 4700 MJMJ with respect to Earth's surface and a kinetic energy of 4400 MJ. Later in its orbit the satellite's potential energy is 5900 MJ. Use conservation of energy to find its kinetic energy at that point.
A satellite at a particular point along an elliptical orbit has a gravitational potential energy of 4700 MJMJ with respect to Earth's surface and a kinetic energy of 4400 MJ. Later in its orbit the satellite's potential energy is 5900 MJ. Use conservation of energy to find its kinetic energy at that point.
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