Orbit altitude, yes; station mass, no.
mv2/r = GMm/r2
m = station mass, cancels out. M = mass of Earth. r = centre of earth to station. G = gravitational constant.
Or, if you assume the station height is negligible compared with the radius of the Earth, then you could use:
v2/r = g (where g = 9.81 m/s2 and r is now just the radius of the Earth).