A satellite of mass m is in a stable circular orbit around the earth at an altitude of…

Physics · JEE Main · NTA ExamsGravitation

A satellite of mass m is in a stable circular orbit around the earth at an altitude of about 100 kilometres. If M is the mass of the earth, R is its radius and g the acceleration due to gravity, the time period T of the revolution of the satellite is given by
  1. \(T=2 \pi \sqrt{\frac{R}{g}}\)
  2. \(T=2 \pi \sqrt{\frac{g}{R}}\)
  3. \(T=2 \pi \sqrt{\frac{M R}{m g}}\)
  4. \(T=2 \pi \sqrt{\frac{m R}{M g}}\)

Answer

(A) T=2 R g

Sign up free on Edukali to view the step-by-step worked solution and practice thousands of similar questions.

Related practice questions

More Gravitation questions · Browse all practice questions