Uses of Package
org.orekit.orbits

Packages that use org.orekit.orbits
Package
Description
This package provides classes relative to the boundary conditions for indirect shooting.
This package provides initial orbit determination methods.
The leastsquares package provides an implementation of a batch least squares estimator engine to perform an orbit determination.
The sequential package provides an implementation of a Kalman Filter engine to perform an orbit determination.
This package contains class managing CCSDS Orbit Data Message.
This package contains class managing CCSDS Orbit Mean-Elements Message.
This package contains class managing CCSDS Orbit Parameter Message.
This package provides interfaces for orbit file representations and corresponding parsers.
This package provides models of simple maneuvers.
This package provides ways to do tessellation and sampling of zones of interest over an ellipsoid surface.
This package provides classes to represent orbits.
Propagation
Top level package for analytical propagators.
This package provides classes to propagate GNSS orbits.
This package provides classes to propagate Intelsat's 11 elements.
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 wraps conversions from an osculating orbit to an averaged state according to a given theory (usually via a fixed-point algorithm using the inverse conversion).
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).
This package provides tools to represent and propagate covariance.
This package provides interfaces and classes dealing with events occurring during propagation.
Utilities for integration-based propagators (both numerical and semi-analytical).
Top level package for numerical propagators.
This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).
This package provides force models for Draper Semi-analytical Satellite Theory (DSST).
This package provides utilities for Draper Semi-analytical Satellite Theory (DSST).
Package specific to calculus assuming a 2D short-term encounter model.
This package provides useful objects.