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Suppose one of the Global Positioning System satellites has a speed of 4.48 km/s at perigee...

Suppose one of the Global Positioning System satellites has a speed of 4.48 km/s at perigee and a speed of 3.20 km/s at apogee. If the distance from the center of the Earth to the satellite at perigee is 2.31×104 km , what is the corresponding distance at apogee?

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Answer #1

For this problem, it is necessary to apply the concepts related to Kepler's second law and the conservation of angular momentum.

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