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Fig. 12

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Semimajor axis (top), eccentricity (middle), and inclination (bottom) as a function of time for a synthetic JFC from Brasser & Morbidelli (2013). The shaded regions indicate where orbital elements are similar to those of P3, where a = aP3 ± 0.1 AU, e = eP3 ± 0.05, and i = iP3 ± 3°. The points where the orbital elements of the synthetic comet meet all these criteria are marked in red.

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