Answer :
For a satellite orbiting around a planet of mass m in an orbit of radius r with a velocity v we have
Fc=Fg
m'v^2/r=G*m*m'/r^2 Where m is the mass of the planet and m' is the mass of satellite
v^2= G*m/r
v=(G*m/r)^1/2
Fc=Fg
m'v^2/r=G*m*m'/r^2 Where m is the mass of the planet and m' is the mass of satellite
v^2= G*m/r
v=(G*m/r)^1/2