Geostationary orbit for Kerbin? :: Kerbal Space Program ...
Place the bus into an eliptical orbit with a period of 2/3 geostationary Ap = 3,463,334.06m Pe = 1,822,703.04m Just before reaching Apoapsis detatch one satelite from the bus and when the sat reaches Apoapsis (3,463,334.06m) circularize its orbit. Next orbit of the bus detach the second sat and circularize it
DA: 95 PA: 60 MOZ Rank: 95