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A satellite is in an elliptical orbit around the earth. The distance from the satellite to...

A satellite is in an elliptical orbit around the earth. The distance from the satellite to the center of the earth ranges from 7.2 Mm at perigee (where the speed is 8.0 km/s) to 9.9 Mm at apogee.

1. Assume the initial conditions are x = 0, y = 7.2 × 106 m, vx = 8.0×103 m/s, and vy = 0. Use python program to print its speed, distance from the earth, kinetic energy, potential energy, and total mechanical energy for each iteration. (What equations should I put in to the program?)

2. Is mechanical energy conserved?

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Expert Solution

genius_generous answered 7 months ago
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