We have been encountering a problem while executing this code
new KeplerianOrbit(15000, 1, 0, 0, 0, 0, PositionAngle.MEAN, FramesFactory.getTOD(false), new AbsoluteDate(2000, 01, 01, 01, 01, 01, TimeScalesFactory.getUTC()), Constants.WGS84_EARTH_MU);
It goes in an endless loop while resolving the kepler equation : it is stucked in KeplerianOrbit.eMeSinE().
We are aware that this orbit is inconsistent but in our use case, orbital parameters come from an external source with possible unexpected set of parameters.
We could ensure consistency of orbital parameters before invoking orekit library but still, we would like to share this problem, if you confirm it is? If so, it should have ended into an OrekitException?