A satellite of mass 2500 kg is orbiting the Earth in an elliptical orbit. At the farthest point
from the Earth, its altitude is 3600 km, while at the nearest point, it is 1100 km. Calculate
the energy and angular momentum of the satellite and its speed at the aphelion and
perihelion.

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Answers

2016-02-21T20:54:21+05:30
Dont forget to mark brilleantest
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