Asked in ETEA MDCAT 2009 2009Moderate

The orbital speed of satellite orbiting around the Earth is:

Correct answer: B. √GMe/Re

  • A. √GM/Re
  • B. √GMe/Re
  • C. √GMe/R²
  • D. √GMe/h

Explanation

The correct formula to calculate the orbital speed (v) of a satellite orbiting the Earth is: v = √(GMe/r) where G is the gravitational constant, Me is the mass of the Earth, and r is the distance between the center of the Earth and the satellite. To derive this formula, we can start with the centripetal force equation F = m v² / r G (Me * m) / r² = m v² / r Solving for v, we get: v = √(GMe/r)

Last updated

About Satellite Motion and Orbital Velocity

Satellite motion uses gravitational force as the centripetal force required for circular orbit, giving relationships among orbital radius, period and orbital velocity. Questions cover geostationary conditions and weightlessness, while distinguishing orbital velocity, escape velocity and the satellite's tangential speed.

Practise Gravitation

265 free Gravitation MCQs from Physics, each with the correct answer and an explanation. Unlimited attempts, no account needed.

Exams that ask Physics questions like this

Physics is on 9 papers prepared for on TestUstad, and all of them draw the same bank, so this question is worth knowing for every one of them.

Related questions