A satellite is orbiting the Earth at an altitude of 400 km. What is its orbital velocity?
Q1. A satellite is orbiting the Earth at an altitude of 400 km. What is its orbital velocity?
Answer: 7.6 km/s
Explanation: The orbital velocity is given by v = √(G * M / (R + h)) = √(g * R² / (R + h)), v ≈ 7.6 km/s.