37 #ifndef _GSATTEME_HPP_
38 #define _GSATTEME_HPP_ 1
41 #include "gVector.hpp"
65 gSatTEME(
const char *pstrName,
char *pstrTleLine1,
char *pstrTleLine2);
148 double tumin, mu, radiusearthkm, xke, j2, j3, j4, j3oj2;
151 std::string m_SatName;
157 #endif // _GSATTEME_HPP_
void setEpoch(gTime ai_time)
Set compute epoch for prediction.
Sat position and velocity predictions over TEME reference system.
gVector getSubPoint()
Get the Geographic satellite subpoint Vector calculated by the method compute SubPoint.
This class implement the needed code to make vector calculations.
gVector getVel()
Get the TEME satellite Velocity Vector.
void setEpoch(double ai_time)
Set compute epoch for prediction.
gVector getPos()
Get the TEME satellite position Vector.
This class implements time calculations.
gSatTEME(const char *pstrName, char *pstrTleLine1, char *pstrTleLine2)
Default class gSatTEME constructor.
void setMinSinceKepEpoch(double ai_minSinceKepEpoch)
Set compute epoch for prediction in minutes since Keplerian data Epoch.