For an eccentric outer body and circular inner perturber, the exterior resonant argument is . At equal mean longitudes , conjunction phases are
The synodic period and coprime determine the visitation order, with advance . For actual true alignment, write and for the eccentric body's true anomaly and mean anomaly. Then instead of . The evenly spaced directions are a leading-small-eccentricity approximation.
In a high-orbital eccentricity interior mean-motion resonance, the resonant argument places successive rotating-frame apocentres at . Avoiding astronomical conjunction at these slow outer excursions favors for and for . This geometrical phase protection suggests stable resonant-argument libration centres; actual dynamical stability requires the resonant perturbation problem.
With constant mean motions and , mean conjunctions advance by each synodic period. Tracking one branch every conjunctions and subtracting gives
The usual formula keeps only first order in . A labelled branch takes to turn once, whereas the full set of interchangeable directions repeats after . Finite orbital eccentricity introduces true-conjunction corrections.
For an exterior circular grain with radiation-pressure coefficient , set and . Its next conjunction occurs after the synodic period, during which the planet's unwrapped mean longitude advances by . A weak planetary scattering encounter changes this by . Unwrapped longitude counts turns; reducing it modulo before comparison would erase this measure of timing sensitivity.

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