Radius of the orbit of a geostationary satellite in terms of g, R and omega

1. A.
   $\left(\frac{gR^2}{\omega^2}\right)^{1/3}$
2. B.
   $\left(\frac{gR^2}{\omega^2}\right)^{2/3}$
3. C.
   $\left(\frac{gR^2}{\omega^2}\right)^{1/2}$
4. D.
   $\frac{gR^2}{\omega^2}$

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1. A.
   $\dfrac{R^2\omega^2}{g}$
2. B.
   $\dfrac{R^2g^2}{\omega^2}$
3. C.
   $\dfrac{R^2g}{\omega}$
4. D.
   $\dfrac{R^2g}{\omega^2}$

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