If the horizontal velocity given to a satellite is greater than critical velocity but less than the escape velocity at the height,then the satellite will

$A$ satellite is orbiting the Earth in a circular orbit of radius $r.$ Which of the following statements is correct?

What are the orbital period of the Moon around the Earth and the rotational period of the Moon about its own axis?

The distance of a geostationary satellite from the surface of the Earth (radius $R_e = 6400 \ km$) in terms of $R_e$ is ....... (in $R_e$)

$A$ planet moving along an elliptical orbit is closest to the sun at a distance $r_1$ and farthest away at a distance of $r_2$. If $v_1$ and $v_2$ are the linear velocities at these points respectively,then the ratio $\frac{v_1}{v_2}$ is

$A$ $10\; kg$ satellite circles Earth once every $2\; hours$ in an orbit having a radius of $8000\; km$. Assuming that Bohr's angular momentum postulate applies to satellites just as it does to an electron in the hydrogen atom, find the quantum number of the orbit of the satellite.