The geostationary orbit of the Earth is at a distance of about 36000 km.
We know that the value acceleration due to gravity above the surface of the Earth is given by .
At h = 36000 km, we have:
At the surface, we have:
For a 120 kg equipment placed in a geostationary satellite, its weight will be
mg' = 120 × 0.233
26.76 ≈ 27 N