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Both orbital eccentricities increase the 6:1 interaction in a coplanar TOI-4600 model

This study tests the source of slow transit timing changes in one model of TOI-4600. It uses the marginal medians in Table 7 of Hu and colleagues, arXiv:2604.26426v1. Newtonian model controls set both orbits in one plane and change their initial eccentricities. With both input eccentricities, the slow timing semi-amplitudes are 42.28 and 62.46 minutes. A Fourier calculation on fixed Kepler ellipses isolates the physical 6:1 interaction. Its amplitude is 9.08 times the sum of the amplitudes with only one eccentric orbit. Mixed eccentricity terms supply the large interaction coefficient in this geometry. A separate control starts with two circular orbits. It retains a 9.23-minute outer timing semi-amplitude. A stellar-motion estimate gives 9.28 minutes. The outer timing RMS falls from 6.50 to 0.058 minutes when the reference changes from the star to the inner center of mass. The slow circular signal is a sampling alias of stellar motion. Independent solver checks and seven public TESS light curves test the calculation. The package contains raw data, model events, code, source records, and three figures. The results apply to this specified model. They do not give a posterior constraint, a new planet, or a transit forecast.

TOI-4600 · transit timing variations · orbital eccentricity · stellar reflex motion · sampling alias · Jacobi coordinates · TESS · reproducible dynamics

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References

10
  1. usesdoi:10.48550/arXiv.2604.26426

    Table 7 of version 1 supplies the fixed model inputs. The public light-curve checks reuse sectors in that study.

  2. doi:10.48550/arXiv.2308.15572

    Original discovery and validation of the two known planets.

  3. supportsdoi:10.3847/0004-637X/821/2/96

    Prior theory gives the dependence of high-order timing signals on both eccentricity vectors.

  4. supportsdoi:10.1111/j.1365-2966.2005.08922.x

    Prior theory describes the timing shift from stellar motion induced by an inner planet.

  5. supportsdoi:10.1088/0004-637X/802/2/116

    Prior theory describes synodic timing terms and sampling aliases.

  6. usesdoi:10.1051/0004-6361/201118085

    REBOUND supplies the orbital initial states and Newtonian integrations.

  7. usesdoi:10.1093/mnras/stu2164

    IAS15 supplies the main numerical integration method.

  8. usesdoi:10.1093/mnras/stv1257

    WHFast supplies a numerical comparison over the full model interval.

  9. usesdoi:10.1086/683602

    batman supplies the local TESS transit profiles.

  10. usesdoi:10.17909/kr6d-vk05

    TESS mission data are accessed through MAST. Exact SPOC product identifiers and hashes are preserved.

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