A planet moving along an elliptical orbit is closest to the Sun at a distance r1 and farthest away at a distance of r2. If v1 and v2 are the linear velocities at these points respectively, then the ratio is:
r1/r2
(r1/r2)2
r2/r1
(r2/r1)2
As we learnt in
Angular momentum of satellite -
Angular momentum
mass of satellite
- wherein
depends on both the masses , mass of centre of body and mass of planet as well as radius of earth.
According to conservation of Angular momentum