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An artificial Earth satellite, of mass 2.00 103 kg, has an elliptical orbit, with a mean altitude of 400 km. (a) What is its mean
An artificial Earth satellite, of mass 2.00 103 kg, has an elliptical orbit, with a mean altitude of 400 km. (a) What is its mean value of gravitational potential energy while in orbit? (b) What is its mean value of orbital kinetic energy? (c) What is its total energy while in orbit?
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