Uses of Interface
org.orekit.data.DataContext

Packages that use DataContext
Package
Description
This package provides interface to represent the position and geometry of space objects such as stars, planets or asteroids.
This package provide base classes for exploring the configured data directory tree and read external data that can be used by the library.
This package provides measurement modifier.
This package contains definitions for CCSDS objects (frames, time systems...).
This package contains the base hierarchy for CCSDS ADM, ODM and TDM.
This package contains class managing CCSDS Attitude Data Message.
This package contains class managing CCSDS Attitude Comprehensive Message.
This package contains class managing CCSDS Attitude Ephemeris Message.
This package contains class managing CCSDS Attitude Parameter Message.
This package contains class managing CCSDS Conjunction Data Message.
This package contains class managing CCSDS Orbit Data Message.
This package contains class managing CCSDS Orbit Comprehensive Message.
This package contains class managing CCSDS Orbit Ephemeris Message.
This package contains class managing CCSDS Orbit Mean-Elements Message.
This package contains class managing CCSDS Orbit Parameter Message.
This package contains class managing CCSDS Tracking Data Message.
This package contains utilities shared by many CCSDS messages parsers/writers.
This package contains classes related to the processing of parse tokens using the state design pattern.
This package provides parsers and writers for Improved Interrange Vector (IIRV) messages.
This package collects classes representing the individual terms that make up an IIRV vector.
This package provides classes to propagate GNSS orbits.
This package provides classes related to navigation data containing in GNSS almanacs and navigation messages.
This package provides classes to read and extrapolate tle's.
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 interfaces and classes dealing with events occurring during propagation.
Top level package for numerical propagators.
Package specific to calculus assuming a 2D short-term encounter model.