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Table 1

Derived orbital solutions.

Object T 0 P γ K e norm log pfalse [10%] log pfalse [1%]
[HJD2 450 000] [d] [km   s-1] [km   s-1] [km   s-1]

HE 14150309 5240.909 ± 0.002 0.192 ± 0.004 104.7 ± 9.5 152.4 ± 11.2 18.6 −1.0 −0.4
HS 2359+1942 6279.221 ± 0.007 0.93261 ± 0.00005 −96.1 ± 6.0 107.4 ± 6.8 8.3 −1.2 −1.1
LB 1516 5495.73 ± 0.05 10.3598 ± 0.0005 14.3 ± 1.1 48.6 ± 1.4 4.4 < −4.0 < −4.0

BPS CS 22879149 5413.102 0.478 21.9 ± 2.5 63.5 ± 2.8 5.4 ... ...
5412.448 0.964 −25.5 ± 5.3 121.7 ± 6.3 6.2 ... ...

OGLE BULSC16 335 4758.614 0.122 36.4 ± 19.6 92.5 ± 26.2 25.1 ... ...
HS 2043+0615 4254.610 ± 0.003 0.3015 ± 0.0003 −43.5 ± 3.4 73.7 ± 4.3 8.3 ... ...
PG 0941+280 4476.185 0.311 73.0 ± 4.9 141.7 ± 6.3 19.4 ... ...
V 1405 Ori 4477.362 0.398 −33.6 ± 5.5 85.1 ± 8.6 15.2 ... ...

Notes. The systematic error adopted to normalise the reduced χ2 (enorm) is given for each case. The probabilities for the orbital period to deviate from our best solution by more than 10% (pfalse [10%]) or 1% (pfalse [1%]) are given in the last columns. The last four lines show the binaries, where the orbital period has been determined from photometry.

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