At height r from the centre of the Earth, orbital velocity is given as:
orbitalvelocity=rGM
Ve=2v
K.E=21m(2v)2=mv2
A satellite is moving with a constant speed v in circular orbit around the earth. An object of mass 'm' is ejected from the satellite such that it just escapes from the gravitational pull of the earth. At the time of ejection, the kinetic energy of the object is:
Held on 10 Jan 2019 · Verified 6 Jul 2026.
23mv2
mv2
21mv2
2mv2
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