$A$ satellite is orbiting around the Earth with an areal speed $v_a$. At what height from the surface of the Earth is it rotating,if the radius of the Earth is $R$?

  • A
    $\frac{4v_a^2}{gR^2} - R$
  • B
    $\frac{2v_a^2}{gR^2} - R$
  • C
    $\frac{v_a^2}{gR^2} - R$
  • D
    $\frac{v_a^2}{2gR^2} - R$

Explore More

Similar Questions

The orbital speed of an artificial satellite very close to the surface of the Earth is $V_o$. What is the orbital speed of another artificial satellite at a height equal to three times the radius of the Earth (in $,V_o$)?

Suppose an astronaut throws a spoon out of a spacecraft. Will the spoon fall to the Earth?

Satellites which give high value data for remote sensing,meteorology and environmental studies are

What are the directions of rotation of a polar satellite and the Earth?

Two satellites $A$ and $B$ are revolving around the earth in orbits of heights $1.25 R_E$ and $19.25 R_E$ from the surface of the earth respectively,where $R_E$ is the radius of the earth. The ratio of the orbital speeds of the satellites $A$ and $B$ is (in $: 1$)

Vedclass Products

For Students

Vedclass Test Series

Mock tests in real JEE/NEET style with performance analysis. 5-day free trial.

Start Free Trial
For Teachers

Exam Paper Generator

Generate Set A/B/C/D exam papers from 7.5L+ questions in 2 minutes. 3 chapters free.

Try Free
For Institutes

Online Exam Module

Live online exams with unlimited students, 360° analytics & white-label branding.

See Demo