4M orbit determination after data processing.
After processing of all the received data, we finally have a very nice parameter set. It has been obtained by the solution of a least cost error function using the dF data that were transmitted by all OM’s that participated and our own received data.
You may download it here:
1 40284U 14065B 14307.75000000 -.00000015 00000-0 -36726+7 0 00002
2 40284 061.6967 069.0661 6145515 000.5872 038.5007 00.07379169000029
The following graph shows the fit of received data (Doppler) and the corresponding Two Lines Elements.
Many thanks to Jean-Baptiste for this wonderful work.