Open Access

Table B.4.

Orbital elements obtained from HERMES or Gaia DR3.

KIC P e ω T0 V0 K f(M) N σ(O − C)
(d) (°) (JD-2 400 000) (km s−1) (km s−1) (10−2 M) (km s−1)
9157260 (O3 - DR3) 675 ± 30 0.30 ± 0.04 313 ± 11 57351 ± 18 −25.7 ± 0.3 8.64 ± 0.41 3.9 ± 1.3 23 -
11394905 (Y4 - DR3) 591 ± 14 0.19 ± 0.09 170 ± 23 57600 ± 35 −71.6 ± 0.2 3.71 ± 0.32 0.30 ± 0.11 22 -
11823838 (Y6 - HER) 915.8 ± 0.6 0.15 ± 0.01 320 ± 3 56103 ± 8 −22.61 ± 0.02 6.09 ± 0.05 2.07 ± 0.05 10 0.04
11823838 (Y6 - DR3) 894 ± 14 0.26 ± 0.04 312 ± 7 57019 ± 16 −22.50 ± 0.16 6.62 ± 0.21 2.4 ± 0.3 23 -
5512910 (Y7 - HER) 1659.5 ± 5.4 0.36 ± 0.03 40 ± 3 59 093 ± 19 −40.35 ± 0.07 3.39 ± 0.07 0.55 ± 0.04 9 0.13
9002884 (Y9 - HER) 593.8 ± 0.8 0.079 ± 0.005 338 ± 7 57533 ± 12 −34.40 ± 0.02 3.94 ± 0.04 0.37 ± 0.01 13 0.07
9002884 (Y9 - DR3) 585 ± 16 0.034 ± 0.064 288 ± 96 57451 ± 155 −34.41 ± 0.16 4.09 ± 0.23 0.41 ± 0.03 21 -
3455760 (Y12 - HER) 918.1 ± 2.8 0.460 ± 0.006 303 ± 1 58753.2 ± 1.7 −46.54 ± 0.01 1.52 ± 0.01 0.0235 ± 0.0007 21 0.08

Notes. P is the orbital period, e is the eccentricity, ω the argument of periastron, T0 the epoch of periastron passage, V0 the velocity of the centre of mass of the system, K the semi-amplitude of the velocity variations, f(M) the mass function, N the number of observations, and σ(O − C) the standard deviation of the O-C (’observed - calculated’) residuals.

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