Uses of Package
org.orekit.propagation.analytical.tle

Package
Description
This package contains class managing CCSDS Orbit Mean-Elements Message.
This package provides classes to read and extrapolate tle's.
This package provides classes related to TLE generation.
This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
This package wraps methods from various (semi)analytical models in Orekit to convert back and forth between an averaged orbital state and an osculating one.
This package provides the ability to convert osculating orbits into mean orbits according to different theories (Brouwer-Lyddane, Eckstein-Hechler, SGP4/SDP4, DSST) with different conversion algorithms (fixed-point, least-squares).