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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


Rita Sharma 7th Dec, 2019
Answer (1)
NAVNEET PANDEY 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

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