Fig. 1.
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Secular trajectories in the TOI-2119 system (Table B.1) adopting P0 = 2.1 day and P1 = 2.0 day. We show the spin axis of the secondary, s1, projected on the orbital plane. These trajectories are obtained by plotting the level curves H0(u, v, x★) = const (Eq. (20)). The stationary solutions (Cassini states) are marked with a dot.
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