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Table 1.

Observational details.

Array Observation Antennas Source Pointing position
Integration Beam size Position rms (a)
date name α2000 δ2000 time angle
(h:m:s) (°:′:″) (h) (mas × mas) (°)
VLBA 27 May 1998 Br, Fd, Hn, Kp, La, Mk, Nl, Ov, Pt, Sc TXS 2226-184 22:29:12.494600 −18:10:47.24200 7.16 1.81 × 0.54 −11.26 5.9 (b), 0.5
VLBA 12 June 2017 Fd, Hn, Kp, La, Mk, Nl, Ov, Pt, Sc TXS 2226-184 22:29:12.494600 −18:10:47.24200 4.13 1.42 × 0.36 −14.72 15.3 (b), 0.4
J2232-1659 (c) 22:32:22.564573 −16:59:01.89226 4.21 1.34 × 0.39 −13.55 1.6
EVN 29 October 2017 Ef, Mc, On, Ys, Hh TXS 2226-184 22:29:12.494600 −18:10:47.24200 2.95 4.16 × 0.97 −26.99 21.7 (b), (d), 0.2
J2232-1659 (c) 22:32:22.564573 −16:59:01.89226 3.04 5.86 × 0.92 −30.28 1.5(e)
EVN 09 June 2018 Ef, Mc, On, Ys, HH, Sr, Jb TXS 2226-184 22:29:12.494600 −18:10:47.24200 3.79 2.11 × 1.41 +7.08 5.1 (b), 0.2

Notes.

(a)

The rms obtained for the radio continuum by averaging the channels that do not show any maser emission is indicated in boldface.

(b)

Measured in channels with no line emission.

(c)

Phase-reference source at 1.4° from TXS 2226-184. The errors of α2000 and δ2000 are 0.291 mas and 0.409 mas, respectively (see Goddard Space Flight Center VLBI group, February 23, 20154).

(d)

The measured rms per channel was 5 mJy beam−1, which needs to be multiplied by the estimated flux correcting factor of 4.35 (see Sect. 3.4).

(e)

The measured rms was 0.34 mJy beam−1, which needs to be multiplied by the estimated flux correcting factor of 4.35 (see Sect. 3.4).

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