getPosition method

Eci getPosition(
  1. double tsince
)

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;
}