Orbital SpeedEasyQuestion 30721
Question
A satellite orbits Earth (mass M, radius R) at height h above surface. Its orbital speed is:
- A√(gR²/(R+h))Correct
- B√(2GM/(R+h))
- C√(GM/R)
- D√(g(R+h))
Correct answer
√(gR²/(R+h))
Explanation
v = √(GM/(R+h)) = √(gR²/(R+h)) since GM = gR².