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A 700-kg satellite is in an elliptical orbit around Earth with a perigee (the point of closest approach) of 7.50 × 106 m from the center of Earth and an apogee (the furthest point from the center of Earth) of 11.5 × 106 m. What is the total energy of the satellite? The mass of Earth is 5.97 × 1024 kg and G = 6.67 x 10-11 N·m2/kg2.
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