1 /* Copyright 2022-2026 Romain Serra
2 * Licensed to CS GROUP (CS) under one or more
3 * contributor license agreements. See the NOTICE file distributed with
4 * this work for additional information regarding copyright ownership.
5 * CS licenses this file to You under the Apache License, Version 2.0
6 * (the "License"); you may not use this file except in compliance with
7 * the License. You may obtain a copy of the License at
8 *
9 * http://www.apache.org/licenses/LICENSE-2.0
10 *
11 * Unless required by applicable law or agreed to in writing, software
12 * distributed under the License is distributed on an "AS IS" BASIS,
13 * WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
14 * See the License for the specific language governing permissions and
15 * limitations under the License.
16 */
17 package org.orekit.orbits;
18
19 /**
20 * Data container for Keplerian orbital elements.
21 * @param a semi-major axis
22 * @param e eccentricity
23 * @param i inclination
24 * @param pa position angle
25 * @param raan right ascension of ascending node
26 * @param anomaly anomaly corresponding to angle type
27 * @param positionAngleType angle type
28 * @author Romain Serra
29 * @see PositionAngleType
30 * @since 14.0
31 */
32 public record KeplerianParameters(double a, double e, double i, double pa, double raan, double anomaly,
33 PositionAngleType positionAngleType) {
34
35 /**
36 * Builds a new instance with the specified position angle type.
37 * @param angleType angle type for the output
38 * @return Keplerian elements with the specified position angle type
39 */
40 public KeplerianParameters withPositionAngleType(final PositionAngleType angleType) {
41 final double convertedAnomaly = KeplerianAnomalyUtility.convertAnomaly(positionAngleType, anomaly, e, angleType);
42 return new KeplerianParameters(a, e, i, pa, raan, convertedAnomaly, angleType);
43 }
44
45 }