1.

A satellite of mass m revolves around the earth of radius R at a height x from its surface. If g is the acceleration due to gravity on the surface of the earth, the orbital speed of the satellite is

A. \[\frac{g{{R}^{2}}}{R+x}\]
B. \[\frac{g{{R}^{2}}}{R-x}\]
C. \[gx\]
D. \[{{\left( \frac{g{{R}^{2}}}{R+x} \right)}^{1/2}}\]
Answer» E.


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