Gnarls B.

asked • 04/26/18

What is the minimum energy that is required to take a stationary satellite...

What minimum energy is required to take a stationary 600 kg satellite from the surface of the moon to an altitude of 9.2x10^5 and put it into an orbit with an orbital speed of 1.36x10^3 m/s?
The thing that I'm really confused about it the calculation for potential energy

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