Explanation on equations please

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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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  • $v_1$ is the escape velocity. If you throw a rock straight upward with this velocity, the rock with escape to infinity.
  • $v$ is the orbital speed for an object to rotate around earth in a circular orbit of radius $R$ without falling back to earth.