java.lang.Object
- java.lang.Enum<OrbitElementsType>
- - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType

All Implemented Interfaces:

Serializable, Comparable<OrbitElementsType>
```
public enum OrbitElementsType
extends Enum<OrbitElementsType>
```
Orbit element set type used in CCSDS Orbit Comprehensive Messages.

Since:

11.0

Author:

Luc Maisonobe

See Also:

SANA registry for orbital elements

Enum Constant Summary

Enum Constants
Enum Constant	Description
`ADBARV`	Spherical 6-element set (α,δ,β,A,r,v).
`CARTP`	Cartesian 3-element position (X, Y, Z).
`CARTPV`	Cartesian 6-element position and velocity (X, Y, Z, XD, YD, ZD).
`CARTPVA`	Cartesian 9-element position, velocity and acceleration (X, Y, Z, XD, YD, ZD, XDD, YDD, ZDD).
`DELAUNAY`	Delaunay elements (L, G, H, l, g, h).
`DELAUNAYMOD`	Modified Delaunay elements (Lm, Gm, Hm, lm, gm, hm).
`EIGVAL3EIGVEC3`	12 elements eigenvalue/eigenvectors (EigMaj, EigMed, EigMin, EigVecMaj, EigVecMed, EigVecMin).
`EQUINOCTIAL`	Equinoctial elements (a, af, ag, L=M+ω+frΩ, χ, ψ, fr).
`EQUINOCTIALMOD`	Modified equinoctial elements (p=a(1−e²), af, ag, L'=υ+ω+frΩ, χ, ψ, fr).
`GEODETIC`	Geodetic elements (λ, ΦGD, β, A, h, vre).
`KEPLERIAN`	Keplerian 6-element classical set (a, e, i, Ω, ω, ν).
`KEPLERIANMEAN`	Keplerian 6-element classical set (a, e, i, Ω, ω, M).
`LDBARV`	Modified spherical 6-element set (λ, δ, β, A, r, v).
`ONSTATION`	Geosynchronous on-station tailored set (a, ex, ey, ix, iy, λ).
`POINCARE`	Canonical counterpart of equinoctial 6-element set (λM=M+ω+Ω, gp, hp, Lp, Gp, Hp).

Method Summary

All Methods Static Methods Instance Methods Concrete Methods
Modifier and Type	Method	Description
`List<Unit>`	`getUnits()`	Get the elements units.
`TimeStampedPVCoordinates`	`toCartesian(AbsoluteDate date, double[] elements, OneAxisEllipsoid body, double mu)`	Convert to Cartesian coordinates.
`double[]`	`toRawElements(TimeStampedPVCoordinates pv, Frame frame, OneAxisEllipsoid body, double mu)`	Convert to raw elements array.
`String`	`toString()`
`static OrbitElementsType`	`valueOf(String name)`	Returns the enum constant of this type with the specified name.
`static OrbitElementsType[]`	`values()`	Returns an array containing the constants of this enum type, in the order they are declared.

Methods inherited from class java.lang.Enum
clone, compareTo, equals, finalize, getDeclaringClass, hashCode, name, ordinal, valueOf

Methods inherited from class java.lang.Object
getClass, notify, notifyAll, wait, wait, wait

- Enum Constant Detail
  - ADBARV
```
public static final OrbitElementsType ADBARV
```
    Spherical 6-element set (α,δ,β,A,r,v).
  - CARTP
```
public static final OrbitElementsType CARTP
```
    Cartesian 3-element position (X, Y, Z).
  - CARTPV
```
public static final OrbitElementsType CARTPV
```
    Cartesian 6-element position and velocity (X, Y, Z, XD, YD, ZD).
  - CARTPVA
```
public static final OrbitElementsType CARTPVA
```
    Cartesian 9-element position, velocity and acceleration (X, Y, Z, XD, YD, ZD, XDD, YDD, ZDD).
  - DELAUNAY
```
public static final OrbitElementsType DELAUNAY
```
    Delaunay elements (L, G, H, l, g, h).
  - DELAUNAYMOD
```
public static final OrbitElementsType DELAUNAYMOD
```
    Modified Delaunay elements (Lm, Gm, Hm, lm, gm, hm).
  - EIGVAL3EIGVEC3
```
public static final OrbitElementsType EIGVAL3EIGVEC3
```
    12 elements eigenvalue/eigenvectors (EigMaj, EigMed, EigMin, EigVecMaj, EigVecMed, EigVecMin).
  - EQUINOCTIAL
```
public static final OrbitElementsType EQUINOCTIAL
```
    Equinoctial elements (a, af, ag, L=M+ω+frΩ, χ, ψ, fr).
  - EQUINOCTIALMOD
```
public static final OrbitElementsType EQUINOCTIALMOD
```
    Modified equinoctial elements (p=a(1−e²), af, ag, L'=υ+ω+frΩ, χ, ψ, fr).
  - GEODETIC
```
public static final OrbitElementsType GEODETIC
```
    Geodetic elements (λ, ΦGD, β, A, h, vre).
  - KEPLERIAN
```
public static final OrbitElementsType KEPLERIAN
```
    Keplerian 6-element classical set (a, e, i, Ω, ω, ν).
  - KEPLERIANMEAN
```
public static final OrbitElementsType KEPLERIANMEAN
```
    Keplerian 6-element classical set (a, e, i, Ω, ω, M).
  - LDBARV
```
public static final OrbitElementsType LDBARV
```
    Modified spherical 6-element set (λ, δ, β, A, r, v).
  - ONSTATION
```
public static final OrbitElementsType ONSTATION
```
    Geosynchronous on-station tailored set (a, ex, ey, ix, iy, λ).
  - POINCARE
```
public static final OrbitElementsType POINCARE
```
    Canonical counterpart of equinoctial 6-element set (λM=M+ω+Ω, gp, hp, Lp, Gp, Hp).
- Method Detail
  - values
```
public static OrbitElementsType[] values()
```
    Returns an array containing the constants of this enum type, in the order they are declared. This method may be used to iterate over the constants as follows:
    for (OrbitElementsType c : OrbitElementsType.values()) System.out.println(c);
    Returns:
    
    an array containing the constants of this enum type, in the order they are declared
  - valueOf
```
public static OrbitElementsType valueOf(String name)
```
    Returns the enum constant of this type with the specified name. The string must match exactly an identifier used to declare an enum constant in this type. (Extraneous whitespace characters are not permitted.)
    
    Parameters:
    
    name - the name of the enum constant to be returned.
    
    Returns:
    
    the enum constant with the specified name
    
    Throws:
    
    IllegalArgumentException - if this enum type has no constant with the specified name
    
    NullPointerException - if the argument is null
  - getUnits
```
public List<Unit> getUnits()
```
    Get the elements units.
    
    Returns:
    
    elements units
  - toCartesian
```
public TimeStampedPVCoordinates toCartesian(AbsoluteDate date,
                                            double[] elements,
                                            OneAxisEllipsoid body,
                                            double mu)
```
    Convert to Cartesian coordinates.
    
    Parameters:
    
    date - elements date
    
    elements - elements values in SI units
    
    body - central body (may be null if type is not GEODETIC)
    
    mu - gravitational parameter in m³/s²
    
    Returns:
    
    Cartesian coordinates
  - toRawElements
```
public double[] toRawElements(TimeStampedPVCoordinates pv,
                              Frame frame,
                              OneAxisEllipsoid body,
                              double mu)
```
    Convert to raw elements array.
    
    Parameters:
    
    pv - Cartesian coordinates
    
    frame - inertial frame where elements are defined
    
    body - central body (may be null if type is not GEODETIC)
    
    mu - gravitational parameter in m³/s²
    
    Returns:
    
    elements elements values in SI units
    
    Since:
    
    12.0
  - toString
```
public String toString()
```
    Overrides:
    
    toString in class Enum<OrbitElementsType>

Enum OrbitElementsType

Enum Constant Summary

Method Summary

Methods inherited from class java.lang.Enum

Methods inherited from class java.lang.Object

Enum Constant Detail

ADBARV

CARTP

CARTPV

CARTPVA

DELAUNAY

DELAUNAYMOD

EIGVAL3EIGVEC3

EQUINOCTIAL

EQUINOCTIALMOD

GEODETIC

KEPLERIAN

KEPLERIANMEAN

LDBARV

ONSTATION

POINCARE

Method Detail

values

valueOf

getUnits

toCartesian

toRawElements

toString