Trajektoori mõõtmise andmeil olid automaatjaama Kuu-lähedase orbiidi parameetrid 29. oktoobril järgmised: minimaalne kaugus Kuu pinnast (periseleen) ligi 100 kilomeetrit, maksimaalne kaugus Kuu pinnast (aposeleen) ligi 1740 kilomeetrit.
The location of the Hold points at the aposelene is selected to be sure that the manoeuvre is passivelysafe, because the chaser must drift away from the target and avoid collisions in the event of failures.
The injected orbit after LOI1 is a moon-centric elliptical orbit with a perilune altitude of 100 km, an apolune altitude of 11800 km, and an inclination of 90 degrees.
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