Table 3: Orbit parameters, for the three different distances. Units: d[kpc], Lz[kpc km s-1], $E_{\rm tot}$[ ${\rm 10 \times km^2~s^{-2}}$], P[Myr], $R_{\rm a}$[kpc], $R_{\rm p}$[kpc], $z_{\rm max}$[kpc], e[pure number].
d Lz $E_{\rm tot}$ P $R_{\rm a}$ $R_{\rm p}$ $z_{\rm max}$ e
3.6 1101 -11085 120 9.50 3.32 0.86 0.48
4.0 1060 -11174 130 9.83 3.09 0.98 0.52
4.4 994 -11232 141 10.12 2.81 1.00 0.56


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