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Table 3.

Morpho-kinematic analysis of [O II] emission.

Coords. RA & Deca PAgasa,b igasa r 1 2 Mathematical equation: $ r_\frac{1}{2} $a,c zsys vrot, gasa,d σv,gasa,d
(J2000) [°] [°] [kpc] [km s−1] [km s−1]
G1 0 h 33 m 40 . s 90 Mathematical equation: $ 0^{\mathrm{h}} 33^{\mathrm{m}} 40{{\overset{\text{ s}}{.}}}90 $ + 2 ° 42 22 . 2 Mathematical equation: $ +2^{\circ}42^{\prime}22{{\overset{\prime\prime}{.}}}2 $e 149.1 ± 0.5 49.5 ± 4.7 7.4 ± 0.01 1.16666 276.8 ± 2.1 26.2 ± 2.5
G2 0 h 33 m 40 . s 92 Mathematical equation: $ 0^{\mathrm{h}} 33^{\mathrm{m}} 40{{\overset{\text{ s}}{.}}}92 $ + 2 ° 42 24 . 3 Mathematical equation: $ +2^{\circ}42^{\prime}24{{\overset{\prime\prime}{.}}}3 $e 43.8 ± 0.7 75.8 ± 0.6 1.6 ± 0.02 1.16745 142.2 ± 2.5 74.2 ± 1.0
G3 0 h 33 m 40 . s 63 Mathematical equation: $ 0^{\mathrm{h}} 33^{\mathrm{m}} 40{{\overset{\text{ s}}{.}}}63 $ + 2 ° 42 24 . 1 Mathematical equation: $ +2^{\circ}42^{\prime}24{{\overset{\prime\prime}{.}}}1 $e 128.1 ± 2.7 42.0 ± 0.0e 2.2 ± 0.09 1.16484 169.9 ± 5.1 < 8.4f

Notes. aDelensed absorber plane. bPosition angle of the approaching semi-major axis (east of north). cHalf-light radius. dAssuming a rotation curve v ( r ) = v rot , gas 2 π arctan ( r / r t ) Mathematical equation: $ v(r) = v_{\mathrm{rot,gas}}\frac{2}{\pi}\arctan(r/r_{\mathrm{t}}) $. eFixed parameter. fUpper limit: The [O II] emission is unresolved at MUSE spectral resolution.

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