1.

What is the total energy possessed by a satellite of mass “m” orbiting above the earth of mass “M” and radius “R” at a height “h”?

A. [(G*M*m)/2*(R+h)]
B. -[(G*M*m)/2*(R+h)]
C. [(G*M*m)/(R+h)]
D. -[(G*M*m)/(R+h)]
Answer» C. [(G*M*m)/(R+h)]


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