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The potential radial orbit accuracy of satellites in low Earth orbits has been investigated through simulation analysis and the reduced dynamic technique. Toward that end, a simulation interface has been developed so that the GIPSY OASIS IP orbit determination software system may be used in simulation analyses. In simulation mode, orbits and measurement data are generated with a given set of models, after which the simulated data are processed with a different set of models. The results are compared to the simulated data, and the difference is due solely to modeling differences and data noise. By introducing model errors of appropriate size, realistic orbit error may be simulated, The simulation technique described has been applied to the GEOSAT Follow-On and TOPEX/Poseidon satellites. The results of the study, incorporating only six ground station into the solution, show that radial orbit accuracy in the GEOSAT orbit will be approximately 4.3 cm rms. When the number of ground tracking stations was increased to 13 and the parameters for the reduced dynamic orbit determination technique were tuned, the radial error was reduced from 4.3 to 3.0 cm in the GEOSAT orbit and from 1.9 to 1.6 cm rms in the TOPEX/Poseidon orbit.