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Table B.2

Median values and 68% confidence intervals of the posterior distributions of the photometric and RV fit of TOI-4342.

Parameter Prior Value
TOI-4342 b Parameters
Orbital period, Pb (days)……. 𝒰(5.40, 5.70) 5.5382592 ± 0.0000034
Transit epoch, T0,b (RJD)……. 𝒰(58653, 58657) 58654.53479-0.00093+0.00084Mathematical equation: $58654.53479_{-0.00093}^{+0.00084}$
Scaled planetary radius, Rp,b/R* 𝒰(0, 0.5) 0.03571-0.00075+0.00073Mathematical equation: $0.03571_{-0.00075}^{+0.00073}$
Impact parameter, bb………. 𝒰(0, 1) 0.382-0.063+0.062Mathematical equation: $0.382_{-0.063}^{+0.062}$
RV semi amplitude, Kb (m/s)… 𝒰(0, 10) 3.78-0.67+0.65Mathematical equation: $3.78_{-0.67}^{+0.65}$
Eccentricity, eb……………. Fixed 0.0
Argument of periastron, ωb (deg) Fixed 90.0
TOI-4342 c Parameters
Orbital period, Pc (days)……. 𝒩(10.60, 10.80) 10.688662 ± 0.000015
Transit epoch, T0,c (RJD)……. 𝒩(58656, 58665) 58659.3486 ± 0.0017
Scaled planetary radius, Rp,c/R* 𝒰(0, 0.5) 0.03602-0.00093+0.00092Mathematical equation: $0.03602_{-0.00093}^{+0.00092}$
Impact parameter, bc………. 𝒰(0, 1) 0.320-0.13+0.12Mathematical equation: $0.320_{-0.13}^{+0.12}$
RV semi amplitude, Kc (m/s)… 𝒰(0, 10) 1.97-0.56+0.57Mathematical equation: $1.97_{-0.56}^{+0.57}$
Eccentricity, ec……………. Fixed 0.0
Argument of periastron, ωc (deg) Fixed 90.0
Candidate d Parameters
Orbital period, Pd (days)……. 𝒰(2, 100) 47.5 ± 1.3
Transit epoch, T0,d (RJD)……. 𝒰(58750, 58850) 58795 ± 27
RV semi amplitude, Kd (m/s)… 𝒰(0, 20) 4.49-0.75+0.73Mathematical equation: $4.49_{-0.75}^{+0.73}$
Eccentricity, ed……………. Fixed 0.0
Argument of periastron, ωd (deg) Fixed 90.0
Stellar parameters
Stellar density, ρ* (ρ)……… 𝒩(2.75, 0.26) 2.86-0.23+0.20Mathematical equation: $2.86_{-0.23}^{+0.20}$
c1,TESS ………………….. N(0.30, 0.10) 0.280 ± 0.081
c2,TESS ………………….. 𝒩(0.34, 0.10) 0.344 ± 0.092
c1,LCO …………………… 𝒩(0.33, 0.10) 0.317 ± 0.087
c2, LCO …………………… 𝒩(0.31, 0.10) 0.297 ± 0.095
Gaussian Process Parameters
A1 (m/s) 𝒰(0, 100) 8.6-1.7+2.4Mathematical equation: $8.6_{-1.7}^{+2.4}$
A2 (m/s) …………………. 𝒰(0, 100) 5.4-1.0+1.4Mathematical equation: $5.4_{-1.0}^{+1.4}$
A3 ……………………… 𝒰(0, 10) 0.49-0.11+0.17Mathematical equation: $0.49_{-0.11}^{+0.17}$
B3 (K) ………………….. 𝒰(0, 10) 6.4-1.9+2.2Mathematical equation: $6.4_{-1.9}^{+2.2}$
Oamp,1 …………………… log 𝒰(0.01, 10) 0.21-0.17+0.14Mathematical equation: $0.21_{-0.17}^{+0.14}$
Oamp,2 …………………… log 𝒰(0.01, 10) 0.048-0.032+0.096Mathematical equation: $0.048_{-0.032}^{+0.096}$
Oamp,3 …………………… log 𝒰(0.01, 10) 3.96 ± 0.70
Pdec (days) ………………. 𝒰(20, 200) 79-13+14Mathematical equation: $79_{-13}^{+14}$
Prot (days) ……………….. 𝒰(10, 100) 14.691-0.070+0.080Mathematical equation: $14.691_{-0.070}^{+0.080}$
Instrument Offsets and Jitters
σRV (m/s) ……………….. 𝒰(0.001, 176)* 2.22-0.41+0.47Mathematical equation: $2.22_{-0.41}^{+0.47}$
μRV (m/s) ……………….. 𝒰(−13950, 6091)* −3922.3 ± 3.2
σBIS (m/s) ………………. 𝒰(0.02, 850)* 1.38-0.9+1.0Mathematical equation: $1.38_{-0.9}^{+1.0}$
μBIS (m/s) ……………….. 𝒰(−10000, 10000)* 39.7-1.8+1.7Mathematical equation: $39.7_{-1.8}^{+1.7}$
σTES S ………………….. 𝒰(0.00, 0.04)* 0.000378-0.000027+0.000029Mathematical equation: $0.000378_{-0.000027}^{+0.000029}$
σΔT4000 K (K) …………….. 𝒰(0.001, 30)* 0.474-0.070+0.077Mathematical equation: $0.474_{-0.070}^{+0.077}$
μΔT4000 K (K) …………….. 𝒰(−10000, 10000)* 1.3-4.4+4.6Mathematical equation: $1.3_{-4.4}^{+4.6}$

Notes. 𝒩(μ, σ2) indicates a normal distribution with mean μ and variance σ2, 𝒰(a, b) a uniform distribution between a and b, log 𝒰(a, b) a log-uniform distribution between a and b. * Automatically determined by PyOrbit.

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