Given that the mass of the earth is 6 x 10^24 and raduis of the earth is 6370000m determine the height above the earths surface for a geostationary satelitte
i know period is 24 hours for a geostationary orbit and i know we need to use keplers law somewhere but i dont how to apply it
i know period is 24 hours for a geostationary orbit and i know we need to use keplers law somewhere but i dont how to apply it