| Satellite Mean Orbital Radius(r) = | m |
| Planet Mass(M) = | kg |
| Satellite Orbit Period(T) = | s |
Universal Gravitational Constant(G) = 6.6726 x 10-11N-m2/kg2
Kepler Third Law (Planetary Motion) to resolve the relationship between the distance of planets from the Sun, and their orbital periods.
Satellite Orbit Period: T = sqrt(4*PI2*r3/GM)
where, r is Satellite Mean Orbital Radius, M is Planet Mass, G is Universal Gravitational Constant equals to 6.6726 x 10-11N-m2/kg2
For example, when r = 5000000m, plant Mass = 2000000000Kg, then satellite orbit period = 192203333768.84s.