Frame referenceFrame
TimeStampedAngularCoordinates orientation
Vector3D center
Vector3D u
Vector3D v
double a
double b
Frame frame
double a2
double b2
double e2
double g
double g2
double evoluteFactorX
double evoluteFactorY
Frame frame
double a
double b
double c
double latitude
double longitude
double altitude
private Object writeReplace()
This intermediate class serializes the files supported names, the ephemeris type and the body name.
Frame bodyFrame
double ae2
double ap2
double f
double e2
double g
double g2
double angularThreshold
double lMe
double lMeDot
double lVe
double lVeDot
double lE
double lEDot
double lMa
double lMaDot
double lJu
double lJuDot
double lSa
double lSaDot
double lUr
double lUrDot
double lNe
double lNeDot
double pa
double paDot
AbsoluteDate date
double tc
double gamma
double gammaDot
double l
double lDot
double lPrime
double lPrimeDot
double f
double fDot
double d
double dDot
double omega
double omegaDot
@DefaultDataContext private Object writeReplace()
This intermediate class serializes only the frame key.
IERSConventions conventions
TimeScale timeScale
double[] lCoefficients
double[] lPrimeCoefficients
double[] fCoefficients
double[] dCoefficients
double[] omegaCoefficients
double[] lMeCoefficients
double[] lVeCoefficients
double[] lECoefficients
double[] lMaCoefficients
double[] lJCoefficients
double[] lSaCoefficients
double[] lUCoefficients
double[] lNeCoefficients
double[] paCoefficients
double[] coefficients
Localizable specifier
Object[] parts
Localizable specifier
Object[] parts
Localizable specifier
Object[] parts
Localizable specifier
String[] parts
Localizable specifier
Object[] parts
Localizable specifier
Object[] parts
double clock
double clockRate
@DefaultDataContext private Object writeReplace()
This intermediate class serializes only the frame key.
IERSConventions conventions
int mjd
AbsoluteDate date
double dt
double lod
double x
double y
double ddPsi
double ddEps
double dx
double dy
ITRFVersion itrfType
@DefaultDataContext private Object writeReplace()
This intermediate class serializes only the frame key.
boolean hasData
EOPHistory.hasDataFor(AbsoluteDate)
IERSConventions conventions
@DefaultDataContext private Object writeReplace()
This intermediate class serializes only the frame key.
Predefined factoryKey
Frame parent
int depth
TransformProvider transformProvider
String name
boolean pseudoInertial
@DefaultDataContext private Object writeReplace()
This intermediate class serializes only the frame key.
IERSConventions conventions
EOPHistory eopHistory
PVCoordinates cartesian
Vector3D rotationVector
Vector3D rotationRate
AbsoluteDate epoch
private Object writeReplace()
This intermediate class serializes only the data needed for generation, but does not serializes the cache itself (in fact the cache is not serializable).
TransformProvider rawProvider
CartesianDerivativesFilter cFilter
AngularDerivativesFilter aFilter
double step
ITRFVersion origin
ITRFVersion destination
TransformProvider provider
Frame frame
CelestialBody primaryBody
CelestialBody secondaryBody
String name
List<E> children
OrphanFrame orphanParent
TransformProvider provider
boolean pseudoInertial
Frame frame
double xp
double yp
private Object writeReplace()
This intermediate class serializes only the data needed for generation, but does not serializes the cache itself (in fact the cache is not serializable).
InterpolatingTransformProvider interpolatingProvider
BodyShape parentShape
GeodeticPoint point
AbsoluteDate date
PVCoordinates cartesian
AngularCoordinates angular
double altitude
double thetamin
double theta0
double elev_star
double refrac_star
double correfrac
double pressure
double temperature
AbsoluteDate defaultDate
Geoid.harmonics
. Used when
no other dates are available. Should be removed in a future release.ReferenceEllipsoid referenceEllipsoid
Vector3D b
double inclination
double declination
double totalIntensity
double horizontalIntensity
double GM
double spin
PVCoordinatesProvider sun
DTM2000InputParameters inputParams
BodyShape earth
TimeScale utc
double n
PVCoordinatesProvider sun
OneAxisEllipsoid earth
double[][] tabAltRho
PVCoordinatesProvider sun
JB2008InputParameters inputParams
BodyShape earth
TimeScale utc
NRLMSISE00InputParameters inputParams
PVCoordinatesProvider sun
BodyShape earth
int[] sw
int[] swc
TimeScale ut
BodyShape shape
double rho0
double h0
double hscale
@DefaultDataContext private Object writeReplace()
Pattern dataPattern
SortedSet<E> data
MarshallSolarActivityFutureEstimation.StrengthLevel strengthLevel
TimeScale utc
AbsoluteDate firstDate
AbsoluteDate lastDate
org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation.LineParameters previousParam
org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation.LineParameters currentParam
@DefaultDataContext private Object writeReplace()
double latitude
double longitude
double r0
double h
double dt
int nbMaps
boolean mapping
AbsoluteDate startDate
AbsoluteDate endDate
Map<K,V> tecMap
TimeScale utc
double[] alpha
double[] beta
TimeScale gps
double[] alpha
double[][] stModip
int month
double[][][] f2
double[][][] fm3
TimeScale utc
GeodeticPoint v0
GeodeticPoint v1
GeodeticPoint v2
GeodeticPoint v3
@DefaultDataContext private Object writeReplace()
This intermediate class serializes all needed parameters,
including position-velocity which are not serialized by parent
Orbit
class.
@DefaultDataContext private Object writeReplace()
double a
double ex
double ey
double i
double raan
double alphaV
double aDot
double exDot
double eyDot
double iDot
double raanDot
double alphaVDot
boolean serializePV
PVCoordinates
serialization.@DefaultDataContext private Object writeReplace()
double a
double ex
double ey
double hx
double hy
double lv
double aDot
double exDot
double eyDot
double hxDot
double hyDot
double lvDot
@DefaultDataContext private Object writeReplace()
double a
double e
double i
double pa
double raan
double v
double aDot
double eDot
double iDot
double paDot
double raanDot
double vDot
Frame frame
AbsoluteDate date
double mu
private Object writeReplace()
int satelliteNumber
char classification
int launchYear
int launchNumber
String launchPiece
int ephemerisType
int elementNumber
AbsoluteDate epoch
double meanMotion
double meanMotionFirstDerivative
double meanMotionSecondDerivative
double eccentricity
double inclination
double pa
double raan
double meanAnomaly
int revolutionNumberAtEpoch
double bStar
String line1
String line2
TimeScale utc
long epoch
Beware, it is not AbsoluteDate.J2000_EPOCH
since it is in TAI and not in TT.
double offset
int year
int month
int day
DateComponents date
TimeComponents time
@DefaultDataContext private Object writeReplace()
int na
int n4
double secInNa
double jd0
double gmst
UTCScale utc
UT1Scale ut1
AbsoluteDate referenceDate
@DefaultDataContext private Object writeReplace()
int weekNumber
double milliInWeek
SatelliteSystem system
AbsoluteDate referenceDate
The reference date is such that the four following instants are equal:
TDBScale tdb
AbsoluteDate referenceDate
The reference date is such that the four following instants are equal:
double ttOffset
TimeScale tt
AbsoluteDate j2000Epoch
int hour
int minute
double second
int minutesFromUTC
Always an integral number of minutes, as per ISO-8601 standard.
UTCScale utc
EOPHistory eopHistory
@DefaultDataContext private Object writeReplace()
org.orekit.time.UTCTAIOffset[] offsets
@DefaultDataContext private Object writeReplace()
Frame frame
double[][] azelmask
double[][] real
double[][] imaginary
double[][] plus
AbsoluteDate date
@DefaultDataContext private Object writeReplace()
AbsoluteDate date
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