A) \[1/{{R}^{2}}\]
B) \[{{R}^{0}}\]
C) \[{{R}^{1}}\]
D) 1/R
Correct Answer: B
Solution :
Gravitational force provides the required centripetal force for orbiting the satellite \[\frac{m{{v}^{2}}}{R}=\frac{K}{R}\] because \[\left( F\propto \frac{1}{R} \right)\] \ \[v\propto R{}^\circ \]
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