Obtain an expression for the orbital velocity and time period of a satellite of mass 'm' revolving around the earth at height 'x' above its surface.
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Explanation:
We have:
R+x
mv
2
=
(R+x)
2
GMm
⇒v=
R+x
GM
=
R
2
GM
×
R+x
R
2
=
R+x
gR
2
because the gravitational force provides the centripetal force for revolution.
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