A satellite is orbiting to the surfqce of the earth, then its speed is
Answers
Answered by
0
- Atmospheric and gravity drag associated with launch typically adds 1.3–1.8 km/s to the launch vehicle delta-v required to reach normal LEO orbital velocity of around 7.8 km/s (28,080 km/h).
The pull of gravity in LEO is only slightly less than on the earth's surface.
Similar questions