Table 1
Parameter selection for the three-body system simulations, categorized based on the choice of the host planet.
| System ID | Planet mass (Mp) | Planet radius (Rp) | Exomoon mass (Mm) | Exomoon radius (Rm) |
|---|---|---|---|---|
| simu 1 | 1 M⊕ | 1 R⊕ | 0.008 M⊕ | 0.25 R⊕ |
| simu 2 | 1 M⊕ | 1 R⊕ | 0.012 M⊕ | 0.27 R⊕ |
| simu 3 | 1 M⊕ | 1 R⊕ | 0.015 M⊕ | 0.29 R⊕ |
| simu 4 | 1 M⊕ | 1 R⊕ | 0.018 M⊕ | 0.38 R⊕ |
| simu 5 | 1 M⊕ | 1 R⊕ | 0.025 M⊕ | 0.41 R⊕ |
| simu 6 | 1 MJ | 1 RJ | 0.008 M⊕ | 0.25 R⊕ |
| simu 7 | 1 MJ | 1 RJ | 0.012 M⊕ | 0.27 R⊕ |
| simu 8 | 1 MJ | 1 RJ | 0.015 M⊕ | 0.29 R⊕ |
| simu 9 | 1 MJ | 1 RJ | 0.018 M⊕ | 0.38 R⊕ |
| simu 10 | 1 MJ | 1 RJ | 0.025 M⊕ | 0.41 R⊕ |
| simu 11 | 1 MJ | 1 RJ | 1 M⊕ | 1 R⊕ |
| simu 12 | 1 MJ | 1 RJ | 1.12 M⊕ | 1.03 R⊕ |
| simu 13 | 1 MJ | 1 RJ | 1.41 M⊕ | 1.10 R⊕ |
| simu 14 | 1 MJ | 1 RJ | 1.78 M⊕ | 1.17 R⊕ |
| simu 15 | 1 MJ | 1 RJ | 2.22 M⊕ | 1.25 R⊕ |
| simu 16 | 1 MJ | 1 RJ | 2.77 M⊕ | 1.32 R⊕ |
| simu 17 | 1 MJ | 1 RJ | 3.43 M⊕ | 1.40 R⊕ |
| simu 18 | 1 MJ | 1 RJ | 4.23 M⊕ | 1.48 R⊕ |
| simu 19 | 1 MJ | 1 RJ | 6.65 M⊕ | 2 R⊕ |
| simu 20 | 1 MJ | 1 RJ | 8.89 M⊕ | 2.5 R⊕ |
| simu 21 | 1 MJ | 1 RJ | 11.26 M⊕ | 3 R⊕ |
| simu 22 | 1 MJ | 1 RJ | 13.76 M⊕ | 3.5 R⊕ |
| simu 23 | 1 MJ | 1 RJ | 16.37 M⊕ | 4 R⊕ |
Notes. All simulated systems adopt a solar-type host star (M⋆ = 1 M⊙ and R⋆ = 1 R⊙). The barycentric orbital periods Pb are sampled between 30 and 365 days, while the moon orbital periods Pm span from 1 to 30 days. Each “system” represents an ensemble of dynamically stable configurations sampled on a 20 × 20 grid in (log Pm, log Pb) space. Stable configurations are defined by orbital distances residing between the Roche limit and 0.4 RHill; unstable systems are removed. The orbital semi-major axes (am, ab) are derived from the sampled periods via Kepler’s third law; consequently, each system is associated with a set of discrete (am, ab) realizations rather than a single unique orbital configuration.
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