Table 4.
Alignment with the VPOS.
| Name | θpred[°] | θobs[°] | p(inVPOS) | p( > VPOS) | p( > obs) |
|---|---|---|---|---|---|
| AquII | 7.8 | −19.6 | 0.532 | 0.449 | 0.709 |
| BooI | 16.1 | −50.5 | 0.057 | 0.004 | 0.000 |
| BooII | 12.8 | −55.8 | 0.014 | 0.001 | 0.000 |
| CVenI | 1.5 | 24.9 | 0.381 | 0.473 | 0.609 |
| CVenII | 4.2 | −7.0 | 0.597 | 0.404 | 0.889 |
| CarI | 4.7 | 8.0 | 1.000 | 0.000 | 0.354 |
| CarII | 3.5 | 43.1 | 0.013 | 0.000 | 0.000 |
| CarIII | 7.1 | 9.8 | 1.000 | 0.000 | 0.015 |
| CBerI | 9.6 | 82.0 | 0.000 | 0.000 | 0.000 |
| CraI | 9.6 | 40.9 | 0.335 | 0.489 | 0.436 |
| CraII | 15.2 | 26.4 | 0.660 | 0.176 | 0.390 |
| DraI | 10.4 | 18.3 | 0.999 | 0.000 | 0.029 |
| DraII | 29.9 | 36.9 | 0.479 | 0.000 | 0.000 |
| EriII | 9.3 | −69.8 | 0.189 | 0.372 | 0.104 |
| FnxI | 14.6 | 28.2 | 0.874 | 0.003 | 0.026 |
| GruI | 24.9 | −89.0 | 0.128 | 0.459 | 0.004 |
| HerI | 37.7 | −37.8 | 0.000 | 1.000 | 0.944 |
| HorI | 1.0 | 4.9 | 0.994 | 0.002 | 0.676 |
| HyaII | 28.9 | 63.7 | 0.145 | 0.600 | 0.199 |
| HyiI | 10.5 | 17.2 | 1.000 | 0.000 | 0.000 |
| LeoI | 20.4 | 88.3 | 0.229 | 0.490 | 0.011 |
| LeoII | 13.4 | 50.4 | 0.388 | 0.556 | 0.393 |
| LeoIV | 2.7 | −58.1 | 0.395 | 0.444 | 0.237 |
| LeoV | 1.1 | −19.3 | 0.401 | 0.621 | 0.795 |
| PhxI | 0.8 | −40.7 | 0.427 | 0.502 | 0.454 |
| PisII | 4.6 | 43.9 | 0.330 | 0.580 | 0.515 |
| RetII | 11.9 | 13.4 | 1.000 | 0.000 | 0.020 |
| SgrI | 60.2 | −76.1 | 0.000 | 1.000 | 0.000 |
| SclI | 5.0 | −7.3 | 1.000 | 0.000 | 0.247 |
| Seg1 | 35.1 | −35.3 | 0.640 | 0.179 | 1.000 |
| Seg2 | 58.7 | −77.9 | 0.000 | 1.000 | 0.000 |
| SxtI | 14.7 | 66.7 | 0.000 | 0.000 | 0.000 |
| TriII | 64.5 | −65.1 | 0.000 | 1.000 | 0.094 |
| TucII | 25.3 | 49.7 | 0.001 | 0.004 | 0.000 |
| TucIII | 6.1 | −16.6 | 0.827 | 0.031 | 0.298 |
| UMaI | 36.0 | −55.1 | 0.001 | 0.555 | 0.003 |
| UMaII | 55.4 | −74.8 | 0.000 | 1.000 | 0.000 |
| UMiI | 21.7 | 29.4 | 0.899 | 0.000 | 0.007 |
| Wil1 | 39.1 | 83.7 | 0.000 | 1.000 | 0.003 |
Notes. Column 1 gives the name of the satellite, Col. 2 the angle between the predicted orbital pole and the VPOS normal, Col. 3 the angle between the median measured orbital pole and the VPOS normal, Col. 4 the fraction of Monte Carlo realizations that have an orbital pole aligned with the VPOS to within the 10% circles, Col. 5 the probability of falsely finding an intrinsically perfectly aligned orbital pole outside of this area given the measurement uncertainties, and Col. 6 the probability of finding an orbital pole at least as far inclined from the VPOS as the median measured orbital pole.
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