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.
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Classes in org.orekit.orbits used by org.orekit.control.indirect.shooting.boundary
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Classes in org.orekit.orbits used by org.orekit.estimation.iodClassDescriptionThis class handles orbital parameters.This class handles orbital parameters.
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Classes in org.orekit.orbits used by org.orekit.estimation.leastsquares
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Classes in org.orekit.orbits used by org.orekit.estimation.sequential
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Classes in org.orekit.orbits used by org.orekit.files.ccsds.ndm.odmClassDescriptionThis class handles traditional Keplerian orbital parameters.Enumerate for true, eccentric and mean position angles.
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Classes in org.orekit.orbits used by org.orekit.files.ccsds.ndm.odm.omm
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Classes in org.orekit.orbits used by org.orekit.files.ccsds.ndm.odm.opmClassDescriptionThis class holds Cartesian orbital parameters.This class handles traditional Keplerian orbital parameters.
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Classes in org.orekit.orbits used by org.orekit.files.general
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Classes in org.orekit.orbits used by org.orekit.forces.maneuversClassDescriptionThis class handles orbital parameters.Enumerate for
OrbitandFieldOrbitparameters types.Enumerate for true, eccentric and mean position angles. -
Classes in org.orekit.orbits used by org.orekit.models.earth.tessellation
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Classes in org.orekit.orbits used by org.orekit.orbitsClassDescriptionAbstract class for orbit interpolator.Abstract class for orbit interpolator.This class holds Cartesian orbital parameters.This class handles circular orbital parameters.This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.This class holds Cartesian orbital parameters.This class handles circular orbital parameters.This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.This class handles traditional Keplerian orbital parameters.Data container for Keplerian orbital elements (Field version).This class handles orbital parameters.This class handles traditional Keplerian orbital parameters.Data container for Keplerian orbital elements.This class handles orbital parameters.Enumerate for
OrbitandFieldOrbitparameters types.This interface represent orbit-like trajectory whose definition is based on a so-called position angle.Enumerate for true, eccentric and mean position angles.Builder for orbits of satellites forming a Walker constellation.Enumerate for Walker constellation design patterns.Container for one satellite slot in aWalker constellation. -
Classes in org.orekit.orbits used by org.orekit.propagationClassDescriptionAbstract class for orbit interpolator.Abstract class for orbit interpolator.This class holds Cartesian orbital parameters.This class holds Cartesian orbital parameters.This class handles orbital parameters.This class handles orbital parameters.Enumerate for
OrbitandFieldOrbitparameters types.Enumerate for true, eccentric and mean position angles. -
Classes in org.orekit.orbits used by org.orekit.propagation.analyticalClassDescriptionThis class holds Cartesian orbital parameters.This class handles circular orbital parameters.This class holds Cartesian orbital parameters.This class handles circular orbital parameters.This class handles traditional Keplerian orbital parameters.This class handles orbital parameters.This class handles traditional Keplerian orbital parameters.This class handles orbital parameters.Enumerate for
OrbitandFieldOrbitparameters types.Enumerate for true, eccentric and mean position angles. -
Classes in org.orekit.orbits used by org.orekit.propagation.analytical.gnssClassDescriptionThis class handles orbital parameters.This class handles orbital parameters.
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Classes in org.orekit.orbits used by org.orekit.propagation.analytical.intelsatClassDescriptionThis class handles orbital parameters.This class handles orbital parameters.
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Classes in org.orekit.orbits used by org.orekit.propagation.analytical.tleClassDescriptionThis class handles orbital parameters.This class handles orbital parameters.
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Classes in org.orekit.orbits used by org.orekit.propagation.analytical.tle.generationClassDescriptionThis class handles traditional Keplerian orbital parameters.This class handles traditional Keplerian orbital parameters.
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Classes in org.orekit.orbits used by org.orekit.propagation.conversionClassDescriptionThis class handles orbital parameters.This class handles orbital parameters.Enumerate for
OrbitandFieldOrbitparameters types.Enumerate for true, eccentric and mean position angles. -
Classes in org.orekit.orbits used by org.orekit.propagation.conversion.averagingClassDescriptionThis class handles orbital parameters.Enumerate for
OrbitandFieldOrbitparameters types.Enumerate for true, eccentric and mean position angles. -
Classes in org.orekit.orbits used by org.orekit.propagation.conversion.averaging.converters
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Classes in org.orekit.orbits used by org.orekit.propagation.conversion.osc2meanClassDescriptionThis class handles orbital parameters.This class handles orbital parameters.
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Classes in org.orekit.orbits used by org.orekit.propagation.covarianceClassDescriptionThis class handles orbital parameters.This class handles orbital parameters.Enumerate for
OrbitandFieldOrbitparameters types.Enumerate for true, eccentric and mean position angles. -
Classes in org.orekit.orbits used by org.orekit.propagation.eventsClassDescriptionThis class handles orbital parameters.This class handles orbital parameters.Enumerate for
OrbitandFieldOrbitparameters types.Enumerate for true, eccentric and mean position angles. -
Classes in org.orekit.orbits used by org.orekit.propagation.integrationClassDescriptionThis class handles orbital parameters.This class handles orbital parameters.Enumerate for
OrbitandFieldOrbitparameters types.Enumerate for true, eccentric and mean position angles. -
Classes in org.orekit.orbits used by org.orekit.propagation.numericalClassDescriptionEnumerate for
OrbitandFieldOrbitparameters types.Enumerate for true, eccentric and mean position angles. -
Classes in org.orekit.orbits used by org.orekit.propagation.semianalytical.dsstClassDescriptionEnumerate for
OrbitandFieldOrbitparameters types.Enumerate for true, eccentric and mean position angles. -
Classes in org.orekit.orbits used by org.orekit.propagation.semianalytical.dsst.forcesClassDescriptionThis class handles orbital parameters.This class handles orbital parameters.
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Classes in org.orekit.orbits used by org.orekit.propagation.semianalytical.dsst.utilitiesClassDescriptionThis class handles orbital parameters.This class handles orbital parameters.
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Classes in org.orekit.orbits used by org.orekit.ssa.collision.shorttermencounter.probability.twodClassDescriptionThis class handles orbital parameters.This class handles orbital parameters.
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Classes in org.orekit.orbits used by org.orekit.utilsClassDescriptionThis class handles orbital parameters.This class handles orbital parameters.Enumerate for
OrbitandFieldOrbitparameters types.Enumerate for true, eccentric and mean position angles.