I am trying to write software in C++, that will transform ECI coordinates of a satellite at a particular time into a point on a 2D map of earth. I know ECI coordinates are easily accessible from TLE data. But it doesn't say anything about what particular latitude and longitude spot on earth the satellite is above.
My question is, how do you know the orientation of the earth at a particular time ( time when TLE was acquired, or in future after orbit propagation ) ? And also, how do you include the effects of precession and nutation when calculating future points, to reach a higher degree of accuracy ? Thank you.