How to use: Step 1: Launch the delivery into a primary parking orbit with an inclination of 0° Step 2: Raise the apoapsis to the height of the targeted orbit Step 3: Raise periapsis, so the orbital period equals 5/6 of the target orbital period (Formula) Step 4: Release one satellite at each apoapsis and circularize its orbit, so you get your satellites evenly distributed around the equator Step 5: Change the inclination of the satellites. Therefore you execute this clockwise every 1/3 period of circulation, so none of the satellites share the same orbital plane but two do share their polar angle. ... Therefore you execute this clockwise every 1/3 period of circulation, so none of the satellites share the same orbital plane but two do share their polar angle. ... What's a 1/3 period of circulation, and how do you judge (or more importantly, measure) it?