In orbit: KE = +GMm/2r, PE = −GMm/r, total E = −GMm/2r (negative = bound). Higher orbit → slower, less bound. Energy of a satellite: kinetic, potential and the bound total.
r = 1.50 R · v = √(GM/r) = 6.5 km/s T = 2π√(r³/GM) = 2.2 h
KE = + · PE = − (MJ/kg-ish) E = −GMm/2r = − (bound)