Q. A satellite orbits the earth 200 km above the surface. What speed, in m/s, is necessary for a circular orbit? The radius of the earth is 6400 km and g = 9.2 m/s2 (Solved)
1. 7200
2. 6600
3. 7800
4. 6000
5. 107 dynes
- c. 7800
1. 7200
2. 6600
3. 7800
4. 6000
5. 107 dynes