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    89.

    A satellite of mass mm is orbiting the earth (of radius RR) at a height hh from its surface. The total energy of the satellite in term of g0{g_0}, the value of acceleration due to gravity at the earth’s surface, is

    A

    βˆ’2mg0R2R+h - \frac{{2m{g_0}{R^2}}}{{R + h}}

    B

    mg0R22(R+h)\frac{{m{g_0}{R^2}}}{{2\left( {R + h} \right)}}

    C

    βˆ’mg0R22(R+h) - \frac{{m{g_0}{R^2}}}{{2\left( {R + h} \right)}}

    D

    Rmg0R2R+h\frac{{Rm{g_0}{R^2}}}{{R + h}}

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