A satellite is in a circular low Earth orbit at an altitude of  390 km  above the equator's surface. For Earth's radius at the equator, use  RE, eq = 6.38 ✕ 106 m. Assuming only the force of Earth's gravity acts on the satellite, determine the smallest required change in the satellite's speed if it is to escape Earth's gravity and never return.

Principles of Physics: A Calculus-Based Text
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Chapter11: Gravity, Planetary Orbits, And The Hydrogen Atom
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A satellite is in a circular low Earth orbit at an altitude of 

390 km

 above the equator's surface. For Earth's radius at the equator, use 

RE, eq = 6.38 ✕ 106 m.



Assuming only the force of Earth's gravity acts on the satellite, determine the smallest required change in the satellite's speed if it is to escape Earth's gravity and never return.

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