Calculate the orbital speed and the escape speed


Suppose a satellite is in a circular orbit 5.425 Earth radii above the surface of the Earth (6.425 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 in km/s? [Hint: You need to calculate the orbital speed and the escape speed.]

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Physics: Calculate the orbital speed and the escape speed
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