For a satellite moving in an orbit around the earth, the ratio of kinetic energy to potential en...
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For a satellite moving in an orbit around the earth, the ratio of kinetic energy to potential energy is :-
(1) 2
(2) \( 1 / 2 \)
(3) \( \frac{1}{\sqrt{2}} \)
(4) \( \sqrt{2} \)
\( \mathrm{P} \)
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