Satellite — Circular OrbitMediumQuestion 30635
Question
For a satellite in circular orbit at radius r, the orbital speed is:
- A√(2GM/r)
- B√(GM/r)Correct
- CGM/r
- D√(gr)
Correct answer
√(GM/r)
Explanation
Gravitational force = centripetal force: GMm/r² = mv²/r → v = √(GM/r).