org.orekit.files.ccsds.ndm.odm.omm

Class OmmTle

java.lang.Object

org.orekit.files.ccsds.section.CommentsContainer

org.orekit.files.ccsds.ndm.odm.omm.OmmTle

All Implemented Interfaces:

Section

public class OmmTle
extends CommentsContainer

Container for TLE data.

Since:

6.1

Author:

sports

Field Summary

Fields

Modifier and Type	Field and Description
static int	EPHEMERIS_TYPE_PPT3 Constant for EPHEMERIS_TYPE PPT3.
static int	EPHEMERIS_TYPE_SGP Constant for EPHEMERIS_TYPE SGP.
static int	EPHEMERIS_TYPE_SGP4 Constant for EPHEMERIS_TYPE SGP4.
static int	EPHEMERIS_TYPE_SGP4_XP Constant for EPHEMERIS_TYPE SGP4-XP.
static int	EPHEMERIS_TYPE_SPECIAL_PERTURBATIONS Constant for EPHEMERIS_TYPE Special Perturbations.

Constructor Summary

Constructors

Constructor and Description
OmmTle() Create an empty data set.

Method Summary

Modifier and Type	Method and Description
double	getAGoM() Get the SGP4-XP solar radiation pressure-like coefficient Aγ/m.
double	getBStar() Get the SGP/SGP4 drag-like coefficient.
double	getBTerm() Get the SGP4-XP drag-like coefficient.
char	getClassificationType() Get the classification type.
int	getElementSetNumber() Get the element set number for this satellite.
int	getEphemerisType() Get the ephemeris type.
double	getMeanMotionDot() Get the first time derivative of the mean motion.
double	getMeanMotionDotDot() Get the second time derivative of the mean motion.
int	getNoradID() Get the NORAD Catalog Number ("Satellite Number").
int	getRevAtEpoch() Get the revolution rumber.
void	setAGoM(double agom) Set the SGP4-XP solar radiation pressure-like coefficient Aγ/m.
void	setBStar(double bstar) Set the SGP/SGP4 drag-like coefficient.
void	setBTerm(double bterm) Set the SGP4-XP drag-like coefficient.
void	setClassificationType(char classificationType) Set the classification type.
void	setElementSetNo(int elementSetNo) Set the element set number for this satellite.
void	setEphemerisType(int ephemerisType) Set the ephemeris type.
void	setMeanMotionDot(double meanMotionDot) Set the first time derivative of the mean motion.
void	setMeanMotionDotDot(double meanMotionDotDot) Set the second time derivative of the mean motion.
void	setNoradID(int noradID) Set the NORAD Catalog Number ("Satellite Number").
void	setRevAtEpoch(int revAtEpoch) Set the revolution rumber.
void	validate(double version) Check is all mandatory entries have been initialized.

Methods inherited from class org.orekit.files.ccsds.section.CommentsContainer

acceptComments, addComment, checkAllowed, checkNotNaN, checkNotNegative, checkNotNull, getComments, refuseFurtherComments

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Field Detail

EPHEMERIS_TYPE_SGP

public static final int EPHEMERIS_TYPE_SGP

Constant for EPHEMERIS_TYPE SGP.

Since:

12.0

See Also:

Constant Field Values

EPHEMERIS_TYPE_SGP4

public static final int EPHEMERIS_TYPE_SGP4

Constant for EPHEMERIS_TYPE SGP4.

Since:

12.0

See Also:

Constant Field Values

EPHEMERIS_TYPE_PPT3

public static final int EPHEMERIS_TYPE_PPT3

Constant for EPHEMERIS_TYPE PPT3.

Since:

12.0

See Also:

Constant Field Values

EPHEMERIS_TYPE_SGP4_XP

public static final int EPHEMERIS_TYPE_SGP4_XP

Constant for EPHEMERIS_TYPE SGP4-XP.

Since:

12.0

See Also:

Constant Field Values

EPHEMERIS_TYPE_SPECIAL_PERTURBATIONS

public static final int EPHEMERIS_TYPE_SPECIAL_PERTURBATIONS

Constant for EPHEMERIS_TYPE Special Perturbations.

Since:

12.0

See Also:

Constant Field Values

Constructor Detail

OmmTle

public OmmTle()

Create an empty data set.

Method Detail

validate

public void validate(double version)

Check is all mandatory entries have been initialized.

This method should throw an exception if some mandatory entries are missing or not compatible with version number.

Specified by:

validate in interface Section

Overrides:

validate in class CommentsContainer

Parameters:

version - format version

getEphemerisType

public int getEphemerisType()

Get the ephemeris type.

Returns:

the ephemerisType

setEphemerisType

public void setEphemerisType(int ephemerisType)

Set the ephemeris type.

Parameters:

ephemerisType - the ephemeris type to be set

getClassificationType

public char getClassificationType()

Get the classification type.

Returns:

the classificationType

setClassificationType

public void setClassificationType(char classificationType)

Set the classification type.

Parameters:

classificationType - the classification type to be set

getNoradID

public int getNoradID()

Get the NORAD Catalog Number ("Satellite Number").

Returns:

the NORAD Catalog Number

setNoradID

public void setNoradID(int noradID)

Set the NORAD Catalog Number ("Satellite Number").

Parameters:

noradID - the element set number to be set

getElementSetNumber

public int getElementSetNumber()

Get the element set number for this satellite.

Returns:

the element set number for this satellite

setElementSetNo

public void setElementSetNo(int elementSetNo)

Set the element set number for this satellite.

Parameters:

elementSetNo - the element set number to be set

getRevAtEpoch

public int getRevAtEpoch()

Get the revolution rumber.

Returns:

the revolution rumber

setRevAtEpoch

public void setRevAtEpoch(int revAtEpoch)

Set the revolution rumber.

Parameters:

revAtEpoch - the Revolution Number to be set

getBStar

public double getBStar()

Get the SGP/SGP4 drag-like coefficient.

Returns:

the SGP/SGP4 drag-like coefficient

setBStar

public void setBStar(double bstar)

Set the SGP/SGP4 drag-like coefficient.

Parameters:

bstar - the SGP/SGP4 drag-like coefficient to be set

getBTerm

public double getBTerm()

Get the SGP4-XP drag-like coefficient.

Returns:

the SGP4-XP drag-like coefficient

Since:

12.0

setBTerm

public void setBTerm(double bterm)

Set the SGP4-XP drag-like coefficient.

Parameters:

bterm - the SGP4-XP drag-like coefficient to be set

Since:

12.0

getMeanMotionDot

public double getMeanMotionDot()

Get the first time derivative of the mean motion.

Returns:

the first time derivative of the mean motion

setMeanMotionDot

public void setMeanMotionDot(double meanMotionDot)

Set the first time derivative of the mean motion.

Parameters:

meanMotionDot - the first time derivative of the mean motion to be set

getMeanMotionDotDot

public double getMeanMotionDotDot()

Get the second time derivative of the mean motion.

Returns:

the second time derivative of the mean motion

setMeanMotionDotDot

public void setMeanMotionDotDot(double meanMotionDotDot)

Set the second time derivative of the mean motion.

Parameters:

meanMotionDotDot - the second time derivative of the mean motion to be set

getAGoM

public double getAGoM()

Get the SGP4-XP solar radiation pressure-like coefficient Aγ/m.

Returns:

the SGP4-XP solar radiation pressure-like coefficient Aγ/m

Since:

12.0

setAGoM

public void setAGoM(double agom)

Set the SGP4-XP solar radiation pressure-like coefficient Aγ/m.

Parameters:

agom - the SGP4-XP solar radiation pressure-like coefficient Aγ/m to be set

Since:

12.0