Earth Observation Mission CFI Software DataHandling Software User Manual for JAVA |
Class for containing data structure for Two Line Elements. More...
Public Member Functions | |
TleRec () | |
Empty constructor. | |
TleRec (String noradSatcat, long satNumber, byte classification, String intDes, double time, double n1st, double n2nd, double bstar, int ephemerisType, int index, int checksum1, double i, double ra, double e, double w, double m, double n, long absOrbit, int checksum2) | |
Constructor with parameters. | |
Public Attributes | |
String | noradSatcat |
Satellite name consistent with the NORAD SATCAT. | |
long | satNumber |
NORAD Catalogue number. | |
byte | classification |
Classification: U=unclassified, S=secret data. | |
String | intDes |
International Designator: (Last two digits of launch year) (Launch number of the year) (Piece of the launch). | |
double | time |
reference time for the element set (UTC processing days MJ2000). | |
double | n1st |
First Time Derivative of the Mean Motion. | |
double | n2nd |
Second Time Derivative of Mean Motion. | |
double | bstar |
BSTAR drag term . | |
int | ephemerisType |
Ephemeris type. | |
int | index |
Element number. | |
int | checksum1 |
Checksum (Modulo 10). | |
double | i |
Inclination [Degrees]. | |
double | ra |
Right Ascension of the Ascending Node [Degrees]. | |
double | e |
Eccentricity. | |
double | w |
Argument of Perigee [Degrees]. | |
double | m |
Mean Anomaly [Degrees]. | |
double | n |
Mean Motion [Revs per day]. | |
long | absOrbit |
Revolution number at epoch [Revs]. | |
int | checksum2 |
Checksum (Modulo 10) (Letters, blanks, periods, plus signs = 0 minus signs = 1). |
Class for containing data structure for Two Line Elements.
EECFI.TleRec.TleRec | ( | ) |
Empty constructor.
EECFI.TleRec.TleRec | ( | String | noradSatcat, | |
long | satNumber, | |||
byte | classification, | |||
String | intDes, | |||
double | time, | |||
double | n1st, | |||
double | n2nd, | |||
double | bstar, | |||
int | ephemerisType, | |||
int | index, | |||
int | checksum1, | |||
double | i, | |||
double | ra, | |||
double | e, | |||
double | w, | |||
double | m, | |||
double | n, | |||
long | absOrbit, | |||
int | checksum2 | |||
) |
Constructor with parameters.
Revolution number at epoch [Revs].
double EECFI.TleRec.bstar |
BSTAR drag term .
Checksum (Modulo 10).
(Letters, blanks, periods, plus signs = 0 minus signs = 1).
Checksum (Modulo 10) (Letters, blanks, periods, plus signs = 0 minus signs = 1).
Classification: U=unclassified, S=secret data.
double EECFI.TleRec.e |
Eccentricity.
Ephemeris type.
double EECFI.TleRec.i |
Inclination [Degrees].
Element number.
String EECFI.TleRec.intDes |
International Designator: (Last two digits of launch year) (Launch number of the year) (Piece of the launch).
double EECFI.TleRec.m |
Mean Anomaly [Degrees].
double EECFI.TleRec.n |
Mean Motion [Revs per day].
double EECFI.TleRec.n1st |
First Time Derivative of the Mean Motion.
double EECFI.TleRec.n2nd |
Second Time Derivative of Mean Motion.
String EECFI.TleRec.noradSatcat |
Satellite name consistent with the NORAD SATCAT.
double EECFI.TleRec.ra |
Right Ascension of the Ascending Node [Degrees].
NORAD Catalogue number.
double EECFI.TleRec.time |
reference time for the element set (UTC processing days MJ2000).
double EECFI.TleRec.w |
Argument of Perigee [Degrees].