I want to have a general solution for calculating orbits. Wikipedia says how to put object on circle orbit. We must give it speed $v_1 = \sqrt{g(h_o +R)} $ Where $h_o$ - is the orbit height, and $R$ - Earth radius.
But how to calculate the speed that the object must have, if we want to place it in an elliptical orbit?
For example:
Having massive massive spherical object with mass $M$ and radius $R$.
which speed $V$ we must to give to this object to put it on elliptical orbit with eccentricity $\epsilon = E$ , and perihelium $P$?