BITSAT2017PhysicsGravitationActual
A geostationary satellite orbits around the earth in a circular orbit of radius 36000 km . Then, the time period of a sky satellite orbiting a few 100 km above the earth's surface R = 64000 km will approximately be
Options
- A1 2   h
- B1   h
- C2   h
- D4   h
Correct answer
C. 2   h
Step-by-step solution
By Kepler's law of planetary motion, T 2 ∝ r 3 , hence T 1 2 ∝ r 1 3 Similarly T 2 2 ∝ r 2 3 ∴   T 1 2 ∝ 36000 3 T 2 2 ∝ 6400 + h 3 Therefore, T 2 2 = T 1 2 6400 + h 36000 3 > T 1 2 6400 3600 3 > 24 2 8 45 3 ∴   T 2 > 24 × 8 × 8 45 × 45 > 1 . 8   h So, T 2 ≅ 2   h