the net force on bodies in stable orbit is nil, the force of gravitational attraction , is balanced by the centripetal force of velocity in a circle.
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example, any orbit radius ( if orbit time not important)
choose your orbit radius, calculate force of gravity, tailor velocity to produce balancing centripital force
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f=((G*m1*m2)/d^2) force of gravity
f = m2 *( v^2/d ) centripetal force
G = newtons constant
m1 = earth mass
m2 = satellite mass
d = orbital distance
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