Orbital Period = Kepler's Third Law P =2*pi*sqrt(a^3/(G*M)), where a =semi-major axis. P =2*pi*sqrt(2.66E8^3 / (8.68E25*6.67428E-11)) P = 358130 - seconds P =358,130 / 3,600 =99.48 - hours
Orbital Period = Kepler's Third Law P =2*pi*sqrt(a^3/(G*M)), where a =semi-major axis. P =2*pi*sqrt(2.66E8^3 / (8.68E25*6.67428E-11)) P = 358130 - seconds P =358,130 / 3,600 =99.48 - hours