A) \[GmM\left( \frac{1}{R_{1}^{2}}-\frac{1}{R_{2}^{2}} \right)\]
B) \[GmM\left( \frac{1}{R_{1}^{{}}}-\frac{1}{R_{2}^{{}}} \right)\]
C) \[2GmM\left( \frac{1}{R_{1}^{{}}}-\frac{1}{R_{2}^{{}}} \right)\]
D) \[\frac{1}{2}GmM\left( \frac{1}{R_{1}^{{}}}-\frac{1}{R_{2}^{{}}} \right)\]
Correct Answer: D
Solution :
The kinetic energy changing the orbit of satellite |
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