Fig. 4

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Examples of capture in secular spin-orbit resonance and tilting to large obliquities. The satellite’s mass and the resonances are labelled as in Fig. 2. Numerical trajectories go from left to right (black dots) over a timespan of billions of years. The migration timescale τ of the satellite is 9 Gyr for panel a and 6 Gyr for panels b and c. Integrations are stopped in the hatched region, where the numerical model used here fails.
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