Stellar motion causes most of the slow outer timing signal in TOI-4600 models with circular initial orbits
Can a slow transit timing signal in TOI-4600 occur when both planets start on circular orbits? We use public mass ratios and orbital elements from Table 7 of Hu et al. (2026). We define a controlled model with both orbits in the same plane and the observer in that plane. We integrate the Newtonian system for 20000 days. The outer planet has a fitted slow timing amplitude of 9.234 minutes at a period of 2954 days. The outer event can also use the center of mass of the star and inner planet as its reference. This change keeps the forces unchanged. It reduces the slow amplitude to 0.045 minute. The star displacement divided by the outer orbital speed predicts 9.279 minutes. Its pointwise estimate agrees with the paired timing shifts to within 0.14 second. Sampling the fast inner orbital motion once per outer orbit produces the slow alias. The inner planet has a fitted slow amplitude below 0.01 minute in this circular initial model. Large slow amplitudes return along a specified path to the published eccentricity components. This contribution tests known timing and sampling effects in specified TOI-4600 models. It includes all event times, code, source checks, and figures. It does not fit observed data or give limits for the true orbital eccentricities.
TOI-4600 · transit timing variations · stellar reflex motion · sampling alias · Jacobi coordinates · reproducible numerical experiment
References
5- usesdoi:10.48550/arXiv.2604.26426
Table 7 of version 1 supplies the stellar mass, planet mass ratios, initial periods, eccentricity components, and conjunction epochs. We use separate marginal medians and change the geometry and initial eccentricities.
- doi:10.1111/j.1365-2966.2005.08922.x
Section 3 gives the known outer transit timing effect from stellar displacement due to an inner planet. We test this mechanism in specified TOI-4600 models.
- doi:10.1088/0004-637X/802/2/116
Section II explains the known frequency alias caused by discrete transit sampling. We apply the sampling identity to the outer transit clock.
- usesdoi:10.1051/0004-6361/201118085
We use REBOUND version 5.2.2 to construct and integrate the three-body models.
- usesdoi:10.1093/mnras/stu2164
IAS15 is the main orbit integrator. A separate Newtonian force function with SciPy DOP853 checks the physical event times.
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