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

210545-q

  • [KVPY 2012]
  • A

    $\frac{v_P}{v_A}=\frac{1+e}{1-e}$

  • B

    $\frac{v_P}{v_A}=1$

  • C

    $\frac{v_P}{v_A}=\frac{1+e^2}{1-e}$

  • D

    $\frac{v_P}{v_A}=\frac{1+e^2}{1-e^2}$

Similar Questions

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

A satellite moves round the earth in a circular orbit of radius $R$ making one revolution per day. A second satellite moving in a circular orbit, moves round the earth once in $8$ days. The radius of the orbit of the second satellite is

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

  • [AIPMT 1994]

The period of revolution of planet $A$ around the sun is $8$ times that of $B$. The distance of $A$ from the sun is how many times greater than that of $B$ from the sun

  • [AIPMT 1997]

An earth satellite $X$ is revolving around earth in an orbit whose radius is one-fourth of the radius of orbit of a communication satellite. Time period of revolution of $X$ is ..........