Two planets at mean distance ${d_1}$ and ${d_2}$ from the sun and their frequencies are $n_1$ and $ n_2$ respectively then
$n_1^2d_1^2 = {n_2}d_2^2$
$n_2^2d_2^3 = n_1^2d_1^3$
${n_1}d_1^2 = {n_2}d_2^2$
$n_1^2{d_1} = n_2^2{d_2}$
Explain Kepler’s first (Law of Orbits) law for planetary motion.
Two satellites are launched at a distance $R$ from a planet of negligible radius. Both satellites are launched in the tangential direction. The first satellite launches correctly at a speed $v_0$ and enters a circular orbit. The second satellite, however, is launched at a speed $\frac {1}{2}v_0$ . What is the minimum distance between the second satellite and the planet over the course of its orbit?
Two heavenly bodies ${S_1}$ and ${S_2}$, not far off from each other are seen to revolve in orbits
A planet is revolving around the sun in a circular orbit with a radius $r$. The time period is $T$. If the force between the planet and star is proportional to $r^{-3 / 2}$, then the square of time period is proportional to
If $r$ denotes the distance between the sun and the earth, then the angular momentum of the earth around the sun is proportional to