A satellite is orbitting around the earth with areal speed $v_a$. At what height from the surface of the earth, it is rotating, if the radius of earth is $R$
A satellite is orbitting around the earth with areal speed $v_a$. At what height from the surface of the earth, it is rotating, if the radius of earth is $R$
- A
$\frac{{4v_a^2}}{{g{R^2}}} - R$
- B
$\frac{{2v_a^2}}{{g{R^2}}} - R$
- C
$\frac{{v_a^2}}{{g{R^2}}} - R$
- D
$\frac{{v_a^2}}{{2g{R^2}}} - R$
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