Orbital Trajectory Correction

機械支援の翻訳下書き (Japanese) for "Orbital Trajectory Correction": Orbital Trajectory Correction is a space maneuver process that adjusts a planned flight path after navigation updates or mission changes for spacecraft orbit planning and station keeping. It uses delta-v estimates, burn timing, and post-maneuver validation so teams can reduce path error before it grows while keeping evidence, reliability, and public-safe operational boundaries clear.

“例文の下書き: The mission team used Orbital Trajectory Correction when a spacecraft entered a crowded orbital shell, so the team could reduce path error before it grows before the next mission decision point.”