MCQ
A satellite of mass $m$ revolves around the earth of radius $R$ at a height $x$ from it's surface. If $g$ is the acceleration due to gravity on the surface of earth, the orbital speed of
- A$gx$
- B${\left( {\frac{{gR}}{{R - x}}} \right)^{1/2}}$
- ✓${\left( {\frac{{gR^2}}{{R + x}}} \right)^{1/2}}$
- D${\left( {\frac{{gR}}{{R + x}}} \right)^{1/2}}$



