Suppose a satellite is in a circular orbit 30 earth radii


Suppose a satellite is in a circular orbit 3.0 Earth radii above the surface of the Earth (3.0 Earth radii from the center of the Earth). By how much does it have to increase its speed in order to be able to escape Earth?

Hint: You need to calculate the orbital speed and the escape speed.

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Physics: Suppose a satellite is in a circular orbit 30 earth radii
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