In page
https://www.orekit.org/static/apidocs/org/orekit/propagation/events/AbstractDetector.html
it is written:
Beware that apside detection will fail for almost circular orbits. If for example an apside detector is used to trigger an
ImpulseManeuver
and the maneuver change the orbit shape to circular, then the detector may completely fail just after the maneuver has been performed!
What is the minimum orbit eccentricity for which this detector won’t fail?
Thank you,
Alfredo