Tracking data from the Tracking and Data Relay Satellite System (TDRSS
) are used to determine operational orbits for a variety of user space
craft. These data are not routinely used for precise orbit determinati
on because the Tracking and Data Relay Satellite (TDRS) orbits, derive
d from Bilateration Ranging Transponder System (BRTS) tracking, are of
insufficient accuracy (40-60 m). Therefore, we have investigated alte
rnative orbit determination techniques to improve our knowledge of TDR
S and user satellite trajectories. These techniques include incorporat
ing ground based tracking of the user satellite, exploiting the enhanc
ed tracking geometry provided by the user satellite, and improving the
force and measurement modeling. Results from analysis of TDRSS-TOPEX/
POSEIDON (T/P) data demonstrate that the TDRSS data are powerful, that
computed TDRS orbits have 3-5 m total position accuracies, and that t
he corresponding T/P ephemerides have 25-40 cm accuracies.