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

double O_SESSAME::tleStruct::bstarDrag

B* drag term (L1) Definition at line 66 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet().

int O_SESSAME::tleStruct::checksumLine1

Checksum for L1 Definition at line 69 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet().

int O_SESSAME::tleStruct::checksumLine2

Checksum for L2 Definition at line 74 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet().

double O_SESSAME::tleStruct::eccentricAnomaly

We calculate Eccentric Anomaly Definition at line 71 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet().

int O_SESSAME::tleStruct::elementNumber

The TLE # (L1) Definition at line 68 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet().

int O_SESSAME::tleStruct::ephemerisType

The type of ephemeris data (L1) Definition at line 67 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet().

double O_SESSAME::tleStruct::epochDay

Epoch day and time for this TLE (L1) Definition at line 63 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet().

int O_SESSAME::tleStruct::epochYear

Epoch year for this TLE (L1) Definition at line 62 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet().

int O_SESSAME::tleStruct::launchNumber

Which launch of that year... (L1) Definition at line 60 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet().

string O_SESSAME::tleStruct::launchPiece

Which piece of that launch... (L1) Definition at line 61 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet().

int O_SESSAME::tleStruct::launchYear

Launched in... (L1) Definition at line 59 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet().

double O_SESSAME::tleStruct::meanAnomaly

The TLE reports Mean Anomaly (L2) Definition at line 70 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet().

double O_SESSAME::tleStruct::meanMotion

We calculate Mean Motion Definition at line 72 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet().

double O_SESSAME::tleStruct::meanmotion1stDeriv

(L1) Definition at line 64 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet().

double O_SESSAME::tleStruct::meanmotion2ndDeriv

(L1) Definition at line 65 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet().

int O_SESSAME::tleStruct::revolutionNumber

How many orbits at epoch? (L2) Definition at line 73 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet().

char O_SESSAME::tleStruct::satClassification

Almost always "U"nclassified (L1) Definition at line 58 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet().

string O_SESSAME::tleStruct::satName

Satellite Name, from Line Zero Definition at line 56 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet().

int O_SESSAME::tleStruct::satNumber

Satellite Number, from Line One Definition at line 57 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet().

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The documentation for this struct was generated from the following file:

• Keplerian.h

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