this is what i wrote:
Orbital velocity is the instantaneous speed in the direction indicated by an arrow drawn as a tangent to the point of interest on the orbital path.
A centripetal force is required to keep an object moving in a circular path. For a planet revolving around the sun in a circular orbit or radius r, the centripetal force is provided by the gravitational attraction between the planet and the sun. If the mass of the planet (satellite) is m and the mass of the sun (central body)is M then:
Fc= mv^2/r
= GmM/r^2
v^2=GM/r
=(2pi r/T)^2
r^3/T^2=GM/4pi^2 (Kepler's Law of Periods)
For any two bodies orbiting the same object, the ratio r^3:T^2 always equals the same fixed value.
The square of a planet's orbital period is proportional to the cube of the mean distance of the planet from the sun.
Feel free to correct me anyone..........