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Table 3

Parameters of the best orbital solution.

Orbital element Value

Date of periastron T0 2 455 328
(2010 May 11)
Period P (years) 6.025
Semi-major axis a (mas) 63.7
Semi-major axis a (AU) 3.2
Eccentricity e 0.755
Argument of periastron ω (°) 253.1
PA of ascending node Ω (°) 36.5
Inclination i (°) 97.5
System mass MAa + Ab (mas3/year2) 7130
Mass error from fit (M)
Mass error from distance error (M) ± 0.097
System mass MAa + Ab (M) 0.90  ±   0.1
reduced χ2 2.1

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