Show that angular momentum of a satellite of mass `M_(s)` revolving around earth of mass `M_(e)` in an orbit of radius `r` is `sqrt(GM_(s)^(2)M_(e)r)`.

Explanation

To show that the angular momentum \( L \) of a satellite of mass \( M_s \) revolving around the Earth of mass \( M_e \) in an orbit of radius \( r \) is given by:

\[ L = \sqrt{G M_s^2 M_e r} \]

we will follow these steps:

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