I have an EARTH ORIENTATION PARAMETERS (EOP) DATA file taken from CelesTrak to convert data from ECI to ECEF. The same file used by STK for the Scenario to be clear.
However its predictions stop at April 2023. I want to extend those values for the next years in the same way STK does. How can I do that?
I've tried by interpolation, the linear interpolation is the one that suits best currently, but when I compare the satellite position e velocity computed by STK in ECEF with mine obtained converting STK's values in ECI to ECEF, the maximum absolute error is of about 20 m.
Thanks in advance!