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Table A.3

Light curve and orbital solutions for our targets.

Parameter LSI+61 145 AN Dor TYC 1881-933-1 HD 254346 TYC 741-1565-1 HD 309317 HD 112485 HD 350685 HD 154407C VI208 Sco
M1(M)-fixed 11.2 8.2 6.6 11 8.8 9 11.6 11.2 11 13.12
Teff1$T_{\rm eff}^1$(K)-fixed 26000 21529 18700 24757 23634 22978 26096 25832 25696 29600
P(d)-fixed 1.846333 2.032883 1.019711 5.431772 2.257173 2.257341 5.372445 2.873794 2.558821 5.219670
γ(kms−1) −36.5±1.9 54.9±2.0 15.1 ±0.4 11.9±2.5 44.3±1.6 −10.3±1.4 −19.3±2.2 20.8±3.0 20.3±1.9 −26.5± 0.3
K1 (km s−1) 22.2±2.8 59.6±2.8 38.7±0.5 15.6±3.8 8.7±2.2 25.6±2.0 55.0±2.8 32.3±5.3 13.2±2.2 44.7±0.4
f(m) (M) 0.00209±0.00079 0.0444±0.0063 0.00612±0.00024 0.00213±0.00155 0.000153±0.000117 0.00393±0.00093 0.0923±0.0139 0.0100±0.0049 0.00060±0.00035 0.0483±0.0013
e-fixed 0 0.052 0 0.015 0 0 0 0 0 0
ω(°) 340.76(fixed) 130.8±1.0
i(°) 81.5±0.05 75.90±0.06 68.07±0.20 76.74±0.10 73.17±0.10 77.60±0.10 78.53±0.15 72.70±0.25 79.14±0.20 85.37±0.20
q-fixed 0.060 0.205 0.113 0.062 0.027 0.082 0.234 0.108 0.040 0.172
M2(M)-fixed 0.67 1.68 0.75 0.68 0.24 0.74 2.71 1.21 0.44 2.26
f1 0.569±0.004 0.676±0.005 0.792±0.003 0.416±0.001 0.602±0.001 0.561 ±0.001 0.412±0.003 0.458±0.007 0.454±0.007 0.359±0.003
f2 0.517±0.001 0.601 ±0.005 0.780±0.002 0.239±0.001 0.422±0.001 0.431 ±0.003 0.289±0.011 0.751 ±0.006 0.463±0.010 0.300±0.005
R1(R) 4.631 ±0.032 4.521 ±0.032 3.468±0.014 6.803±0.015 5.441 ±0.008 4.742±0.008 6.141 ±0.042 4.782±0.070 4.704±0.073 5.632±0.047
R2(R) 1.221 ±0.002 1.948±0.016 1.293±0.003 1.140±0.005 0.808±0.002 1.195±0.008 2.206±0.080 2.912±0.023 1.178±0.025 2.108±0.035
Teff2$T_{\rm eff}^2$ (K) 8082-10286±500 9071-9941 ±150 8671-9826± 120 11680-12327±50 8295-10319± 175 7777-9430±150 13625-14017± 100 8074-9536±150 14214-14784±300 12252-12951 ±400
Prot (d) 2.12±0.03 1.37±0.01 1.14±0.17 1.67 ±0.02 1.77 ±0.07 1.15±0.01 1.66±0.08 0.93±0.02 1.61 ±0.09 3.27±0.30
log(g1) 4.16±0.01 4.04±0.01 4.18±0.01 3.81±0.01 3.91 ±0.01 4.04±0.01 3.93±0.01 4.13±0.01 4.43± 4.05±0.01
log(g2) 4.09±0.01 4.08±0.01 4.09±0.01 4.16±0.01 4.00±0.01 4.15±0.01 4.18±0.03 3.59±0.01 3.94±0.02 4.14±0.01

Notes. The RV solution for AN Dor comes from Table 1 and that of V1208 Sco from Banyard et al. (2022) - see text for details. For the other targets, the zero point γ and amplitude K1 were calculated assuming zero eccentricity with the period and To from Table A.2. To calculate the photometric solutions of all targets, we fixed the eccentricities and ephemerides (Table A.2), primary masses and primary effective temperatures (from Table A.1), and mass ratios (derived from the mass functions f(m) and a preliminary fitting to get inclinations i). For secondary temperatures, the first value provides the usual effective temperatine (i.e., without any reflection effect) while the second value corresponds to a mean over the stellar surface, that is, it accounts for the heating of some parts of the star because of the reflection effect. The rotation period Prot is calculated using 2πR1 sin(i)/νsin(i).

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