Step 1:
According to Kepler's third law, the period of a planet or satellite is given by the equation:
\[t = \frac{2\pi}{\sqrt{GM_s}} \cdot r^{3/2}\]
where \(t\) is the period, \(G\) is the gravitational constant, \(M_s\) is the mass of the satellite, and \(r\) is
Show more…