Geostationary satellites maintain a fixed position over a certain point over the equator so they are always able to communicate with the same area on the surface of the Earth. The Earth's mass is $\backslash (5\mathrm{.}97\backslash$times $10^\{24\}\backslash$mathrm$\{$~kg$\}\backslash )$ and you can assume it is a sphere. If the satellite needs to make a full revolution in $24$ h $,$ what is the distance between the satellite and the Earth's center?