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Energy of Satellite

A space station orbits around the Earth at the height "h" above the Earth's surface . A small satellite of mass m is launched from the space station to arrive at a geostationary orbit, such that the satellite is constantly above a fixed location on earth surface.

**Find the energy required to launch the satellite .( mass of earth "M" , radius "R" and angular velocity "w"(omega), gravitational constant G )

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