getPosition method
getPosition() This procedure returns the ECI position and velocity for the satellite at "tsince" minutes from the (GMT) TLE epoch. The vectors returned in the ECI object are kilometer-based. tsince - Time in minutes since the TLE epoch (GMT).
Implementation
Eci getPosition(double tsince) {
Eci? eci = m_pNoradModel.getPosition(tsince);
eci!.ae2Km();
return eci;
}