The time period of a satellite, revolving above earth’s surface at a height equal to \( R \), will be:(Given: \( g = \pi^2 \, \text{m/s}^2 \), \( R \) = radius of earth).
\( \sqrt{32R} \)
\( \sqrt{4R} \)
\( \sqrt{8R} \)
\( \sqrt{2R} \)