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  1. The mean radius of earth is R, its angular speed on its own axis is ω and the acceleration due to gravity at earth's surface is g. What will be the radius of the orbit of a geostationary satellite ?
    1. (​R2g / ω​2)1 / 3
    2. (​Rg / ω​2)1 / 3
    3. (​R2 ω​2 / g)1 / 3
    4. (​R2g / ω​)1 / 3
Correct Option: A

T =
2πr
=
2πr
=
2πr3 / 2
=
v0(gR2 / r)1 / 2(gR2)1 / 2ω

Hence , r3 / 2 =
gR²
or r3 =
gR2
ωω2

or r = (gR2 / ω2)1 / 3



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