Table 2: Elements of the orbit.
P = $370.5 \pm 0.5$ d

T = $2449215.69 \pm 1.94$ d

e = $0.62 \pm 0.04$

v = $-0.52 \pm 0.36$ km s^-1

$\omega_1$ = $191.7 \pm 5.4^{o}$

K = $11.35 \pm 0.81$ km s^-1

$a\sin i$ = $(45.2~\pm 5.4)~10^{6}$ km

f_m = $0.0268 \pm 0.0095$ $M_{\odot}$

$\sigma$ = 2.24 km s^-1

**Table 2:** Elements of the orbit.
P	=	$370.5 \pm 0.5$ d
T	=	$2449215.69 \pm 1.94$ d
e	=	$0.62 \pm 0.04$
v	=	$-0.52 \pm 0.36$ km s^-1
$\omega_1$	=	$191.7 \pm 5.4^{o}$
K	=	$11.35 \pm 0.81$ km s^-1
$a\sin i$	=	$(45.2~\pm 5.4)~10^{6}$ km
f_m	=	$0.0268 \pm 0.0095$ $M_{\odot}$
$\sigma$	=	2.24 km s^-1

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