Radius of orbit of satellite of earth is $R$. Its kinetic energy is proportional to
$\frac{1}{R}$
$\frac{1}{{\sqrt R }}$
$R$
$\frac{1}{{{R^{3/2}}}}$
Radius of orbit of satellite of earth is $R$. Its kinetic energy is proportional to
$K.E. = \frac{{GMm}}{{2R}}$
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