geostationary satellite
We know that generally for geostationary station T=24 hours, h=3.6x10⁴km, R=6400 km, and velocity is 3.1 km/s. I think this values are stationary for geostationary satellite.
Let we want to place a geostationary station for which h= 300 km. Which steps should be taken to place this satellite in this height? If it is possible, please say details about the solution of that problem.
