O_SESSAME::tleStruct Struct Reference

#include <Keplerian.h>

List of all members.

Public Attributes
string	satName
int	satNumber
char	satClassification
int	launchYear
int	launchNumber
string	launchPiece
int	epochYear
double	epochDay
double	meanmotion1stDeriv
double	meanmotion2ndDeriv
double	bstarDrag
int	ephemerisType
int	elementNumber
int	checksumLine1
double	meanAnomaly
double	eccentricAnomaly
double	meanMotion
int	revolutionNumber
int	checksumLine2

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Member Data Documentation

string O_SESSAME::tleStruct::satName

Satellite Name, from Line Zero Definition at line 40 of file Keplerian.h.

int O_SESSAME::tleStruct::satNumber

Satellite Number, from Line One Definition at line 41 of file Keplerian.h.

char O_SESSAME::tleStruct::satClassification

Almost always "U"nclassified (L1) Definition at line 42 of file Keplerian.h.

int O_SESSAME::tleStruct::launchYear

Launched in... (L1) Definition at line 43 of file Keplerian.h.

int O_SESSAME::tleStruct::launchNumber

Which launch of that year... (L1) Definition at line 44 of file Keplerian.h.

string O_SESSAME::tleStruct::launchPiece

Which piece of that launch... (L1) Definition at line 45 of file Keplerian.h.

int O_SESSAME::tleStruct::epochYear

Epoch year for this TLE (L1) Definition at line 46 of file Keplerian.h.

double O_SESSAME::tleStruct::epochDay

Epoch day and time for this TLE (L1) Definition at line 47 of file Keplerian.h.

double O_SESSAME::tleStruct::meanmotion1stDeriv

(L1) Definition at line 48 of file Keplerian.h.

double O_SESSAME::tleStruct::meanmotion2ndDeriv

(L1) Definition at line 49 of file Keplerian.h.

double O_SESSAME::tleStruct::bstarDrag

B* drag term (L1) Definition at line 50 of file Keplerian.h.

int O_SESSAME::tleStruct::ephemerisType

The type of ephemeris data (L1) Definition at line 51 of file Keplerian.h.

int O_SESSAME::tleStruct::elementNumber

The TLE # (L1) Definition at line 52 of file Keplerian.h.

int O_SESSAME::tleStruct::checksumLine1

Checksum for L1 Definition at line 53 of file Keplerian.h.

double O_SESSAME::tleStruct::meanAnomaly

The TLE reports Mean Anomaly (L2) Definition at line 54 of file Keplerian.h.

double O_SESSAME::tleStruct::eccentricAnomaly

We calculate Eccentric Anomaly Definition at line 55 of file Keplerian.h.

double O_SESSAME::tleStruct::meanMotion

We calculate Mean Motion Definition at line 56 of file Keplerian.h.

int O_SESSAME::tleStruct::revolutionNumber

How many orbits at epoch? (L2) Definition at line 57 of file Keplerian.h.

int O_SESSAME::tleStruct::checksumLine2

Checksum for L2 Definition at line 58 of file Keplerian.h.

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