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Table 4

Initial conditions for orbit calculations derived from the mean values of observational input data (Table 3), together with standard deviations of their distributions.

x σx y σy z σz vx σvx vy σvy vz σv z
[kpc] [kpc] [kpc] [km s-1] [km s-1] [km s-1]

7.05 0.04 –3.70 0.13 0.76 0.03 –39.7 2.7 –197.7 1.3 –12.1 2.6

Notes. See Sect. 3.1 for the description of the used coordinate system.

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