Question: A satellite orbits the Earth in a circular orbit of radius r. At some point its rocket engine is fired so that its speed increases
A satellite orbits the Earth in a circular orbit of radius r. At some point its rocket engine is fired so that its speed increases rapidly by a small amount. As a result, do the
(a) Apogee distance and
(b) Perigee distance increase, decrease, or stay the same?
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