what will be the velocity of a satellite revolving around the earth at a height h above surface of earth if radius of earth is R
Answer (1)
7th Dec, 2019
Hello Rita
The answer for this question will be
V= √GM/R.
Where v is the velocity.
g is gravitational constant.
M is the mass
And R is the radius.
And there also Kepler's formula for this you can read that too.
I hope it helps
Comments (0)
Related Questions
Trending Articles/News
