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)]