A satellite orbiting Earth has a tangential velocity of 5000 m/s. Earth’s mass is 6 × 1024 kg and its radius is 6.4 × 106 m
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ME x G/ (rE)² = ω²r
ME is the mass of the earth
G = gravitational constant = 6.6742 x 10-11 m3 s-2 kg-1
Re is the radius of the earth
ω is the angular velocity
and r is the orbit's radius
In order to convert to angular velocity:
Tangential velocity = rω
ω = 5000/r
(6x10²⁴) x (6.6742 x 10⁻¹¹) /(6.4 x 10⁶)²
= (5000/r)²r
r = 2557110.465 m
So the distance is 2.6 x 10^6 m
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