A satellite moves in a circular orbit of radius 8.0 × 106 m around the Earth (mass 5.97 × 1024 kg). What is its orbital speed?
- Gravitational force = centripetal force: GMm/r2 = mv2/r, so v2 = GM/r.
- GM = 6.67 × 10−11 × 5.97 × 1024 = 3.98 × 1014 N m2 kg−1.
- v2 = 3.98 × 1014 ÷ 8.0 × 106 = 4.98 × 107 m2 s−2.
- v = √(4.98 × 107) = 7.06 × 103 m s−1.
Answer: About 7.1 × 103 m s−1.