Package org.orekit.propagation.conversion

This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator. The conversion principle is to minimize the mean square error for positions and velocities over a given time span.

The conversion from osculating to mean elements appears as a side effect of propagation models conversion.

These package extends an original contribution from Telespazio for TLE (Orbit Converter for Two-Lines Elements) to all propagators.

Pascal Parraud