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Table 1

Derived orbital solutions, mass functions and minimum companion masses.

Object T 0 a P a γ a K a e norm f(M) M 2 b i max c
[2 450 000] [d] [km s-1] [km s-1] [km s-1] [M] [M] °

CPD-64°481 3431.5796 ± 0.0002 0.27726315 ± 0.00000008 93.54 ± 0.06 23.81 ± 0.08 0.16 0.0004 >0.048 70
PHL 457 5501.5961 ± 0.0009 0.3131 ± 0.0002 20.7 ± 0.2 13.0 ± 0.2 0.7 0.00007 >0.027 75

Notes.

(a)

The systematic error adopted to normalise the reduced χ2 (enorm) is given for each case.

(b)

The minimum companion masses take into account the highest possible inclination.

(c)

i = 90 is defined as an edge-on orbit.

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