Final orbit-fit solution for NSB. Least-squares propagated formal uncertainties are derived using a nonlinear mapping of the covariance matrix (CM) based on a MCCM/RP method. Uncertainties based on the Jackknife resampling method are also presented. Geocentric positional differences in the ICRF are presented in right ascension (α), declination (δ), and range (D) directions. The norm of the 3D differences (Δd) are also shown. Exc. means excluding, V2 3D means Voyager 2 3D, Occ. means occultation, Rel. means relative, Mer. means meridian, Pho. means photographic, and Obs. means observations.