We know that the centripetal force required to hold the object in a circular orbit is provided by the gravitational force between the object and the planet. We write this fact as the equation
where M, m and r are the massof the planet and of the satellite and the radius of the orbit about the planet's center.
Solving for the planet mass M, we obtain
We know r, and G is the universal gravitational constant, so if we can find the velocity v of the orbit object, we can find the mass M of the planet.
- circumference = distance = `ds = 2 `pi ( 20000 km).
- v = 24060 m/s.
Substituting into the expression M = v ^ 2 r / G, we find that the massof the planet is
To find planetary mass from the orbital radius and period of a small satellite we solve the orbital condition m v^2 / r = G M m / r^2 for M to obtain
then determine v from the orbital circumference and period. We obtain
where T is the period of the orbit.
Substituting this expression for v into M = v^2 r / G we obtain