Year 3, Day 254: ROKSAT IIIYear 3, Day 277: ROKSAT IVAn initial 34m/s burn at apoapsis places the satellite into a stable orbit. A 122m/s burn at periapsis pushes the orbit to the target periapsis height. Then, at apoapsis, the satellite circularizes into a transfer orbit. A final 94m/s burn places the satellite into the intended orbit.
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