Two satellites A & B go around the earth in circular orbits at a height of${\text{R}}_{\text{A}}\&{\text{R}}_{\text{B}}$ respectively from the surface of the earth. Assume earth to be a uniform sphere of radius${\text{R}}_{\text{e}}$ . The ratio of the magnitudes of the velocities of the satellite $\frac{{\text{V}}_{\text{A}}}{{\text{V}}_{\text{B}}}$ is