I've got seemingly two different equations for velocity in orbit:
$$v_1 = \sqrt{ \frac{2GM}{R}} $$
and $$v = \sqrt{ \frac{Gm_e}{R}}$$
What is the difference between these two? I'm quite sure that $G$ is the gravitational constant, $m_e$ is the mass of the earth. $R$ is the radius of orbit in both cases. I'm not sure what the sub script $1$ is but it has something to do with energy conservation.
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