Fig. 1


Upper panel: Euclidean error norm of various orbital solutions with respect to the multi-arc ESOC reference. Lower panel: residuals with respect to the Earth-bound range of the orbital solutions. r0 is the purely gravitational solution, rMarsden a Marsden-type orbit, and robs the best-fit reconstructed orbit for the non-gravitational acceleration shown in Fig. 2. The shaded band indicates thevariation across 31 initial positions for the Marsden solution.

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