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Physics, 24.02.2020 16:56 hctlawton

The altitude of a satellite in an elliptical orbit around the earth is 1600 km at apogee and 600 km at perigee. Determine the: a) eccentricity of the orbit b) velocities at perigee and apogee c) time required to go from perigee to apogee

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The altitude of a satellite in an elliptical orbit around the earth is 1600 km at apogee and 600 km...
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