#include <Keplerian.h>
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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B* drag term (L1) Definition at line 66 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet(). |
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Checksum for L1 Definition at line 69 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet(). |
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Checksum for L2 Definition at line 74 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet(). |
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We calculate Eccentric Anomaly Definition at line 71 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet(). |
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The TLE # (L1) Definition at line 68 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet(). |
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The type of ephemeris data (L1) Definition at line 67 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet(). |
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Epoch day and time for this TLE (L1) Definition at line 63 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet(). |
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Epoch year for this TLE (L1) Definition at line 62 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet(). |
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Which launch of that year... (L1) Definition at line 60 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet(). |
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Which piece of that launch... (L1) Definition at line 61 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet(). |
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Launched in... (L1) Definition at line 59 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet(). |
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The TLE reports Mean Anomaly (L2) Definition at line 70 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet(). |
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We calculate Mean Motion Definition at line 72 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet(). |
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Definition at line 64 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet(). |
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Definition at line 65 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet(). |
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How many orbits at epoch? (L2) Definition at line 73 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet(). |
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Almost always "U"nclassified (L1) Definition at line 58 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet(). |
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Satellite Name, from Line Zero Definition at line 56 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet(). |
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Satellite Number, from Line One Definition at line 57 of file Keplerian.h. Referenced by O_SESSAME::Keplerian::ReadTwoLineElementSet(). |