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OREKIT (ORbits Extrapolation KIT) is a low level space dynamics library.
It provides basic elements (orbits, dates, attitude, frames ...) and
various algorithms to handle them (conversions, analytical and numerical
propagation, pointing ...).
/* Copyright 2002-2024 CS GROUP
* Licensed to CS GROUP (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
* (the "License"); you may not use this file except in compliance with
* the License. You may obtain a copy of the License at
*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS,
* WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
* See the License for the specific language governing permissions and
* limitations under the License.
*/
package org.orekit.bodies;
import java.io.Serializable;
import org.orekit.frames.Frame;
import org.orekit.utils.ExtendedPVCoordinatesProvider;
/** Interface for celestial bodies like Sun, Moon or solar system planets.
* @author Luc Maisonobe
* @see CelestialBodyFactory
*/
public interface CelestialBody extends Serializable, ExtendedPVCoordinatesProvider {
/** Get an inertially oriented, body centered frame.
* The frame is always bound to the body center, and its axes have a
* fixed orientation with respect to other inertial frames.
* @return an inertially oriented, body centered frame
* @see #getBodyOrientedFrame()
*/
Frame getInertiallyOrientedFrame();
/** Get a body oriented, body centered frame.
* The frame is always bound to the body center, and its axes have a
* fixed orientation with respect to the celestial body.
* @return a body oriented, body centered frame
* @see #getInertiallyOrientedFrame()
*/
Frame getBodyOrientedFrame();
/** Get the name of the body.
* @return name of the body
*/
String getName();
/** Get the attraction coefficient of the body.
* @return attraction coefficient of the body (m³/s²)
*/
double getGM();
}