Help about estimated propagator by orbit determination

Orekit usage
3

Hi @lirw1984,

I’ve tried to reproduce your results but I’m missing the SINEX files for the station positions.
Could you please share them?

I don’t have an answer yet to your issue but it reminds me of this one: Re-computed estimated measurements.

I don’t think it will change a lot but, in your input file, could you try replacing:

# Propagator definition
propagator:
  # Numerical integrator (min step (s), max step (s) and position error (m))
  integrator:
    minStep: 0.001
    maxStep: 300
    positionError: 10.0

With:

# Propagator definition
propagator:
  # Numerical integrator (min step (s), max step (s) and position error (m))
  integrator:
    minStep: 0.001
    maxStep: 60.
    positionError: 0.001

And tell us how it compares with this configuration ?