A planet orbits in an elliptical path of eccentricity $e$ around a massive star considered fixed at one of the foci. The point in space, where it is closest to the star is denoted by $P$ and the point, where it is farthest is denoted by $A$. Let $v_P$ and $v_A$ be the respective speeds at $P$ and $A$, then
$\frac{v_P}{v_A}=\frac{1+e}{1-e}$
$\frac{v_P}{v_A}=1$
$\frac{v_P}{v_A}=\frac{1+e^2}{1-e}$
$\frac{v_P}{v_A}=\frac{1+e^2}{1-e^2}$
The satellite of mass $m$ revolving in a circular orbit of radius $r$ around the earth has kinetic energy $E$. Then its angular momentum will be
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The distance of neptune and saturn from sun are nearly ${10^{13}}$ and ${10^{12}}$ meters respectively. Assuming that they move in circular orbits, their periodic times will be in the ratio
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