If $L$ is the angular momentum of a satellite revolving around earth is a circular orbit of radius $r$ with speed $v$, then .........
$L \propto v$
$L \propto r$
$L \propto \sqrt{r}$
$L \propto \sqrt{v}$
The time period of an artificial satellite in a circular orbit of radius $R$ is $2\, days$ and its orbital velocity is $v_0$. If time period of another satellite in a circular orbit is $16 \,days$ then
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
A geostationary satellite is at a height $h$ above the surface of earth. If earth radius is $R$
What is the direction of areal velocity of the earth around the sun ?
If satellite is shifted towards the earth. Then time period of satellite will be