Objective: orbit validations of TOPEX/Poseidon POE routinely computed by CNES and GSFC.
Principal Parameters: Computations have been performed using ITRF 97 reference frame Orbits from GSFC and CNES have been used for input
Results can be compared to those obtain with ITRF 96 reference frame (results availables only for cycles 1 to 272). Subscribe to
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