Exchange of ejecta between Telesto and Calypso: Tadpoles, horseshoes, and passing orbits
Anthony R. Dobrovolskis, Jose' Luis Alvarellos, Kevin J. Zahnle, and, Jack J. Lissauer

TL;DR
This study numerically investigates the orbital dynamics of ejecta from Saturn's Trojan moons Telesto and Calypso, revealing distinct trajectories and timescales for re-impact and escape based on launch velocities and directions.
Contribution
It provides a detailed classification of ejecta trajectories around Tethys' Trojan moons, including tadpole, horseshoe, and passing orbits, with implications for surface and orbital evolution.
Findings
Ejecta re-impact times range from less than a day to several thousand years.
Most ejecta with passing orbits are accreted by Tethys within a few years.
Ejecta can be scattered to other moons like Enceladus and Dione.
Abstract
We have numerically integrated the orbits of ejecta from Telesto and Calypso, the two small Trojan companions of Saturn's major satellite Tethys. Ejecta were launched with speeds comparable to or exceeding their parent's escape velocity, consistent with impacts into regolith surfaces. We find that the fates of ejecta fall into several distinct categories, depending on both the speed and direction of launch. The slowest ejecta follow sub-orbital trajectories and re-impact their source moon in less than one day. Slightly faster debris barely escape their parent's Hill sphere and are confined to tadpole orbits, librating about Tethys' triangular Lagrange points L4 (leading, near Telesto) or L5 (trailing, near Calypso) with nearly the same orbital semi-major axis as Tethys, Telesto, and Calypso. These ejecta too eventually re-impact their source moon, but with a median lifetime of a few…
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