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Table 4.

Orbital parameters for J1022−3414.

Parameter Value Parameter Value
X [kpc] 8 . 31 0.06 + 0.07 Mathematical equation: $ -8.31^{+0.07}_{-0.06} $ Xf [kpc] 8 . 37 0.05 + 0.06 Mathematical equation: $ -8.37^{+0.06}_{-0.05} $
Y [kpc] 3 . 52 3.58 + 0.77 Mathematical equation: $ -3.52^{+0.77}_{-3.58} $ Yf [kpc] 6 . 10 3.56 + 0.76 Mathematical equation: $ -6.10^{+0.76}_{-3.56} $
Z [kpc] 1 . 32 0.36 + 1.16 Mathematical equation: $ 1.32^{+1.16}_{-0.36} $ Zf [kpc] 0 . 00 0.10 + 0.10 Mathematical equation: $ 0.00^{+0.10}_{-0.10} $
r [kpc] 9 . 09 0.39 + 1.89 Mathematical equation: $ 9.09^{+1.89}_{-0.39} $ rf [kpc] 10 . 32 0.47 + 2.36 Mathematical equation: $ 10.32^{+2.36}_{-0.47} $
VX [km s−1] 20 . 0 6.7 + 11.2 Mathematical equation: $ 20.0^{+11.2}_{-6.7} $ VX, f [km s−1] 7 10 + 16 Mathematical equation: $ 7^{+16}_{-10} $
VY [km s−1] 814 58 + 160 Mathematical equation: $ 814^{+160}_{-58} $ VY, f [km s−1] 809 62 + 156 Mathematical equation: $ 809^{+156}_{-62} $
VZ [km s−1] 406 140 + 468 Mathematical equation: $ 406^{+468}_{-140} $ VZ, f [km s−1] 411 141 + 462 Mathematical equation: $ 411^{+462}_{-141} $
vgrf [km s−1] 872 87 + 410 Mathematical equation: $ 872^{+410}_{-87} $ vgrf, f [km s−1] 873 96 + 404 Mathematical equation: $ 873^{+404}_{-96} $
vgrf − vesc [km s−1] 271 99 + 423 Mathematical equation: $ 271^{+423}_{-99} $ vej [km s−1] 716 108 + 474 Mathematical equation: $ 716^{+474}_{-108} $
Boundness [%] 0 tflight [Myr] 2 . 74 0.16 + 0.35 Mathematical equation: $ 2.74^{+0.35}_{-0.16} $

Notes. Quoted uncertainties correspond to the 1σ confidence intervals.

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