What is the station's orbital speed? The radius of Earth is 6.37×106m, its mass is 5.98×10^24kg.
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).
I think we will need the mass of 'the station' and orbit altitude to answer this question....
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).
Which makes sense ...explains how multiple sattellites of different masses can all be placed in 'stationary' orbits above the eqauator and do not crash into each other....