The following information shows the result of the orbit fit based on Gary Bernstein's method. Most of the information should be self-explanatory. Take special note that while the original Bernstein software works with barycentric coordinates, we convert these results into a heliocentric coordinate system.
# Object: 11UX410
# Created Thu Apr 18 01:13:51 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 34 observations of 34
# Arc: 9.14y
# First observation: 2011/08/30
# Last observation: 2020/10/20
# Chi-squared of fit: 15.70 DOF: 62 RMS: 0.12
# Min/Max residuals: -0.35 0.33
# Exact a, adot, b, bdot, g, gdot:
1.616631E-05 2.772570E-02 -4.285801E-06 -8.514748E-03 2.800383E-02 -9.051914E-03
# Covariance matrix:
1.6555E-13 -3.0225E-14 -4.9157E-15 6.9331E-15 1.2091E-13 -7.5392E-14
-3.0225E-14 1.1755E-13 1.7043E-14 -3.6311E-14 4.6212E-14 4.1923E-13
-4.9157E-15 1.7043E-14 5.6052E-14 -1.5110E-14 5.1230E-15 6.4902E-14
6.9331E-15 -3.6311E-14 -1.5110E-14 1.9548E-14 -1.5154E-14 -1.3840E-13
1.2091E-13 4.6212E-14 5.1230E-15 -1.5154E-14 1.7462E-13 1.8053E-13
-7.5392E-14 4.1923E-13 6.4902E-14 -1.3840E-13 1.8053E-13 1.5980E-12
# lat0 lon0 xBary yBary zBary JD0
3.561641 34.081811 0.849627 0.033513 -0.538913 2455804.016986
# Heliocentric elements and errors
Epoch: 2455804.5000 = 2011/08/31
Mean Anomaly: 303.23524 +/- 0.007
Argument of Peri: 262.52133 +/- 0.007
Long of Asc Node: 223.98431 +/- 0.000
Inclination: 17.44139 +/- 0.000
Eccentricity: 0.32841972 +/- 0.0000
Semi-Major Axis: 39.64545066 +/- 0.0027
Time of Perihelion: 2470181.3853 +/- 8.1
Perihelion: 26.62510274 +/- 0.0026
Aphelion: 52.66579857 +/- 0.0041
Period (y) 249.6308 +/- 0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X 30.44547047 +/- 0.0004
Ecliptic Y 19.57211805 +/- 0.0003
Ecliptic Z 2.21822106 +/- 0.0000
Ecliptic XDOT -0.00221087 +/- 0.0000
Ecliptic YDOT 0.00178449 +/- 0.0000
Ecliptic ZDOT -0.00088577 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 36.26195111 +/- 0.0004
Geocenter to KBO 35.70960818 +/- 0.0005
# Hcoef: 8.26
The following table shows the complete astrometric record for 11UX410. The first three columns show the date of observation. The next six columns are RA and DEC. The next column (when provided) is the observed magnitude and filter. The next column is the object name (11UX410) followed by the observatory code and reference code for the source of the astrometry.
2011 08 30.51622 02 02 18.557 +16 13 42.96 24.2r 11UX410 568 C~1C6M 2011 08 30.56278 02 02 18.431 +16 13 42.37 24.1r 11UX410 568 C~1C6M 2011 08 30.60922 02 02 18.311 +16 13 41.78 23.9r 11UX410 568 C~1C6M 2011 09 05.61026 02 02 01.556 +16 12 14.36 23.9r 11UX410 568 C~1C6M 2011 10 25.31577 01 58 12.363 +15 50 01.33 11UX410 568 C~1C6M 2011 10 25.31577 01 58 12.35 +15 50 01.2 24.1r 11UX410 568 C~3j8g 2011 10 25.36423 01 58 12.100 +15 49 59.59 23.6r 11UX410 568 C~1C6M 2011 10 25.41871 01 58 11.796 +15 49 57.86 23.5r 11UX410 568 C~1C6M 2011 10 25.41871 01 58 11.80 +15 49 58.0 23.1r 11UX410 568 C~3j8g 2011 10 25.47315 01 58 11.492 +15 49 55.95 23.6r 11UX410 568 C~1C6M 2011 10 25.47315 01 58 11.48 +15 49 55.8 23.6r 11UX410 568 C~3j8g 2011 10 26.26973 01 58 07.172 +15 49 28.64 23.6r 11UX410 568 C~1C6M 2011 10 26.32241 01 58 06.883 +15 49 26.87 23.7r 11UX410 568 C~1C6M 2011 10 26.32241 01 58 06.86 +15 49 26.7 11UX410 568 C~3j8g 2011 10 26.36558 01 58 06.645 +15 49 25.43 23.7r 11UX410 568 C~1C6M 2011 10 31.30918 01 57 39.799 +15 46 34.83 11UX410 568 C~1C6M 2011 10 31.35747 01 57 39.535 +15 46 33.12 23.7r 11UX410 568 C~1C6M 2011 10 31.37121 01 57 39.468 +15 46 32.62 23.8r 11UX410 568 C~1C6M 2011 12 01.32447 01 55 08.282 +15 29 08.64 23.7r 11UX410 568 C~1C6M 2012 01 26.31723 01 53 50.429 +15 12 12.27 23.7r 11UX410 568 C~1C6M 2012 01 27.25145 01 53 52.013 +15 12 10.64 24.1r 11UX410 568 C~1C6M 2012 08 23.54195 02 09 31.133 +16 19 45.67 24.0r 11UX410 568 C~1C6M 2012 08 24.57765 02 09 29.245 +16 19 35.98 23.9r 11UX410 568 C~1C6M 2012 10 21.33175 02 05 32.636 +15 57 05.96 23.5r 11UX410 568 C~1C6M 2012 10 21.35746 02 05 32.488 +15 57 05.12 23.5r 11UX410 568 C~1C6M 2012 10 21.38354 02 05 32.343 +15 57 04.22 23.6r 11UX410 568 C~1C6M 2013 01 14.34100 02 00 28.538 +15 18 37.53 23.8r 11UX410 568 C~1C6M 2013 02 02.25091 02 00 52.166 +15 17 25.19 23.9r 11UX410 568 C~1C6M 2013 02 03.25659 02 00 54.541 +15 17 27.26 23.9r 11UX410 568 C~1C6M 2013 11 01.47101 02 11 43.34 +15 55 27.6 11UX410 568 C~1CKy 2013 11 01.48128 02 11 43.28 +15 55 27.3 11UX410 568 C~1CKy 2013 11 01.49156 02 11 43.23 +15 55 27.0 11UX410 568 C~1CKy 2020 10 20.431020 03 07 22.051 +16 05 55.69 23.5G 11UX410 G37 C~4KuJ 2020 10 20.499070 03 07 21.680 +16 05 53.67 11UX410 G37 C~4KuJ
The following table shows the residuals to the orbit fit. The first coumn is the point number. The second column is the time, in years, measured from the first observation. The third and fifth columns are the regularized positions used in the orbit fit. The fourth and sixth columns are the residuals, in arc seconds, for RA and Dec respectively.
1 0.0000 0.00 -0.06 0.00 -0.14
2 0.0001 0.00 -0.13 0.00 -0.13
3 0.0003 0.00 -0.10 0.00 -0.12
4 0.0167 0.00 0.09 0.00 -0.05
5 0.1528 0.00 -0.21 0.00 -0.01
6 0.1528 0.00 -0.01 0.00 0.12
7 0.1529 0.00 0.07 0.00 0.02
8 0.1531 0.00 0.10 0.00 0.29
9 0.1531 0.00 0.04 0.00 0.15
10 0.1532 0.00 -0.17 0.00 -0.05
11 0.1532 0.00 0.01 0.00 0.10
12 0.1554 0.00 -0.02 0.00 0.05
13 0.1555 0.00 -0.34 0.00 -0.10
14 0.1555 0.00 0.01 0.00 0.07
15 0.1556 0.00 0.02 0.00 0.10
16 0.1692 0.00 -0.04 0.00 0.07
17 0.1693 0.00 -0.02 0.00 0.02
18 0.1693 0.00 0.11 0.00 -0.00
19 0.2541 0.00 0.06 0.00 0.04
20 0.4074 0.00 0.03 0.00 -0.17
21 0.4100 0.00 0.20 0.00 0.13
22 0.9830 0.00 0.33 0.00 -0.17
23 0.9858 0.00 0.08 0.00 -0.10
24 1.1439 0.00 0.07 0.00 -0.00
25 1.1440 0.00 -0.01 0.00 0.01
26 1.1441 0.00 -0.00 0.00 -0.03
27 1.3767 0.00 0.06 0.00 0.11
28 1.4284 0.00 -0.08 0.00 -0.18
29 1.4312 0.00 -0.03 0.00 -0.35
30 2.1737 0.00 -0.10 0.00 0.02
31 2.1738 0.00 -0.13 0.00 0.07
32 2.1738 0.00 -0.01 0.00 0.12
33 9.1415 0.00 -0.07 0.00 0.01
34 9.1416 0.00 0.08 0.00 0.02
The following table comes from a 10My integration of the orbit of the object. Three columns are shown. The first column is the result of integrating the nominal orbit. The other two columns are based on clones of the nominal orbit that are +/- 3 sigma from the nominal orbit. If all three types agree then the classificiation is deemed secure. The basis for these calculations is described in more detail in AJ, 129, 1117 (2005). Any use made of these calculations should refer to and credit this publication and the Deep Ecliptic Survey Team.
11UX410 quality flag:3 Type: 3:2E 3:2E 3:2E axisobj 39.715 39.715 39.715 ecceobj 0.327 0.327 0.328 incobj 17.423 17.423 17.423 qmin 25.960 25.961 25.960 qmax 53.496 53.497 53.495 amean 39.454 39.454 39.454 amin 39.061 39.061 39.061 amax 39.933 39.932 39.933 emean 0.266 0.266 0.266 emin 0.158 0.158 0.158 emax 0.340 0.340 0.340 imean 20.890 20.890 20.890 imin 17.497 17.497 17.498 imax 24.348 24.348 24.349 excite_mean 0.448 0.448 0.448 fracstop 1.000 1.000 1.000 cjmean 2.821 2.821 2.821 libcent 0 177.6 177.8 177.5 libamp 0 52.7 52.8 52.6 libcent 1 -180.0 -180.0 -180.0 libamp 1 -180.0 -180.0 -180.0 libcent 2 -180.0 -180.0 -180.0 libamp 2 -180.0 -180.0 -180.0 libcent 3 -180.0 -180.0 -180.0 libamp 3 -180.0 -180.0 -180.0 libcent 4 -180.0 -180.0 -180.0 libamp 4 -180.0 -180.0 -180.0 kozaimean 265.0 265.0 265.0 kozaiamp 76.7 76.7 76.7