The potential energy of a satellite of mass \( m \) revolving around the earth at a height of \( R \) from the surface of the earth is:
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Gravitational potential energy at a height \(h\) is given by \( U = - \frac{GMm}{R + h} \). If the height is equal to the radius of the earth, the potential energy becomes \( -0.5mgR_e \).
The gravitational potential energy of a satellite at height \(h\) is given by:
\[
U = - \frac{GMm}{R + h}.
\]
Here \( R \) is the radius of the earth, and \( h = R \). Substituting \(h = R\) into the formula:
\[
U = - \frac{GMm}{2R}.
\]
Since \(GM = g R^2\), the potential energy becomes:
\[
U = -0.5mgR_e.
\]
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