A satellite of mass m is orbiting the earth (of radius R) at a height h from its surface. The total energy of the satellite in terms of g0, the value of acceleration due to gravity at the earth's surface, is

  • -2mg0R2/R+h
  • mg0R2/2(R+h)
  • -mg0R2/2(R+h)
  • Rmg0R2/R+h
  • Explanation:

    TE = GMm/2(R+h) = -GMm/2(R+h) R2/R2 = g0mR2/2(R+h)

A satellite of mass m is orbiting the earth (of radius R) at a height h from its surface. The total
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