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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 $$g_0$$, the value of acceleration due to gravity at the earth's surface, is
$$-\frac{mg_0R^2}{2(R+h)}$$
$$\frac{2mg_0R^2}{R+h}$$
$$-\frac{2mg_0R^2}{R+h}$$
$$\frac{mg_0R^2}{2(R+h)}$$
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