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: 591392 # Created Sat May 4 01:09:09 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 80 observations of 80 # Arc: 11.15y # First observation: 2010/06/21 # Last observation: 2021/08/16 # Chi-squared of fit: 68.75 DOF: 154 RMS: 0.16 # Min/Max residuals: -0.64 0.50 # Exact a, adot, b, bdot, g, gdot: 1.657520E-05 2.663264E-02 -3.143380E-06 -1.366123E-03 2.533580E-02 2.285407E-03 # Covariance matrix: 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 # lat0 lon0 xBary yBary zBary JD0 -8.393599 -22.009292 0.941984 -0.054975 -0.372169 2455369.122656 # Heliocentric elements and errors Epoch: 2455368.5000 = 2010/06/21 Mean Anomaly: 21.30316 +/- 0.000 Argument of Peri: 220.95787 +/- 0.000 Long of Asc Node: 87.36382 +/- 0.000 Inclination: 8.87857 +/- 0.000 Eccentricity: 0.14486267 +/- 0.0000 Semi-Major Axis: 45.89355388 +/- 0.0000 Time of Perihelion: 2448648.5265 +/- 0.0 Perihelion: 39.24529125 +/- 0.0000 Aphelion: 52.54181651 +/- 0.0000 Period (y) 310.9107 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 36.20155511 +/- 0.0000 Ecliptic Y -15.64878835 +/- 0.0000 Ecliptic Z -5.76158715 +/- 0.0000 Ecliptic XDOT 0.00128644 +/- 0.0000 Ecliptic YDOT 0.00259086 +/- 0.0000 Ecliptic ZDOT -0.00018213 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 39.85761960 +/- 0.0000 Geocenter to KBO 39.46980294 +/- 0.0000 # Hcoef: 6.56
The following table shows the complete astrometric record for 591392. 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 (591392) followed by the observatory code and reference code for the source of the astrometry.
2010 06 21.62189 22 51 37.094 -16 20 37.64 21.7G 591392 F51 C~346I 2010 09 15.30046 22 46 29.803 -17 00 29.68 22.7G 591392 F51 C~346I 2011 08 24.43675 22 54 22.111 -16 18 50.72 22.1G 591392 F51 C~346I 2011 08 24.45075 22 54 22.044 -16 18 51.24 22.7G 591392 F51 C~346I 2011 08 24.46471 22 54 21.970 -16 18 51.60 22.8G 591392 F51 C~346I 2011 08 24.47869 22 54 21.910 -16 18 52.08 23.2G 591392 F51 C~346I 2012 08 14.48350 23 01 06.279 -15 42 10.01 22.8G 591392 F51 C~346I 2012 08 14.49855 23 01 06.229 -15 42 10.77 22.4G 591392 F51 C~346I 2012 08 14.51360 23 01 06.139 -15 42 11.10 22.7G 591392 F51 C~346I 2012 08 14.52863 23 01 06.097 -15 42 11.82 21.8G 591392 F51 C~346I 2013 08 09.44969 23 07 26.647 -15 07 03.16 22.9G 591392 F51 C~346I 2013 08 09.46393 23 07 26.596 -15 07 03.74 22.5G 591392 F51 C~346I 2013 08 09.47818 23 07 26.534 -15 07 03.92 22.5G 591392 F51 C~346I 2013 08 09.49242 23 07 26.482 -15 07 04.53 22.6G 591392 F51 C~346I 2013 08 26.47023 23 06 12.275 -15 16 03.38 22.6G 591392 F51 C~346I 2013 08 26.48127 23 06 12.182 -15 16 03.24 21.2G 591392 F51 C~346I 2013 08 26.49643 23 06 12.143 -15 16 04.04 22.0G 591392 F51 C~346I 2013 08 26.50878 23 06 12.103 -15 16 04.41 23.2G 591392 F51 C~346I 2013 08 30.44922 23 05 53.689 -15 18 05.83 21.5G 591392 F51 C~346I 2013 09 01.42444 23 05 44.371 -15 19 06.15 22.6G 591392 F51 C~346I 2013 09 01.43865 23 05 44.304 -15 19 06.58 22.6G 591392 F51 C~346I 2013 09 01.45211 23 05 44.247 -15 19 07.11 22.6G 591392 F51 C~346I 2013 09 01.46556 23 05 44.179 -15 19 07.53 22.5G 591392 F51 C~346I 2013 09 22.40301 23 04 05.387 -15 28 41.46 22.2G 591392 F51 C~346I 2013 09 22.41117 23 04 05.356 -15 28 42.01 22.0G 591392 F51 C~346I 2013 10 24.25359 23 02 01.711 -15 37 12.21 22.6G 591392 F51 C~346I 2013 10 24.26467 23 02 01.654 -15 37 12.39 21.1G 591392 F51 C~346I 2014 06 24.62017 23 15 09.794 -14 14 19.81 20.7G 591392 F51 C~346I 2014 08 28.40632 23 12 00.072 -14 44 14.52 22.5G 591392 F51 C~346I 2014 08 28.41686 23 12 00.033 -14 44 14.91 22.5G 591392 F51 C~346I 2014 08 28.42739 23 11 59.944 -14 44 15.25 21.7G 591392 F51 C~346I 2014 09 17.44147 23 10 25.659 -14 54 00.27 22.2G 591392 F51 C~346I 2014 09 17.45417 23 10 25.636 -14 54 00.98 22.6G 591392 F51 C~346I 2014 09 17.46848 23 10 25.551 -14 54 01.35 21.6G 591392 F51 C~346I 2014 09 17.48120 23 10 25.511 -14 54 01.83 21.5G 591392 F51 C~346I 2014 09 19.37384 23 10 16.650 -14 54 50.90 22.8G 591392 F51 C~346I 2014 09 19.38383 23 10 16.601 -14 54 51.14 22.5G 591392 F51 C~346I 2014 09 19.39384 23 10 16.538 -14 54 51.61 22.5G 591392 F51 C~346I 2014 09 19.40382 23 10 16.512 -14 54 52.00 22.5G 591392 F51 C~346I 2014 11 22.23808 23 07 02.291 -15 04 40.18 22.7G 591392 F51 C~346I 2014 11 24.20590 23 07 01.395 -15 04 18.63 22.9G 591392 F51 C~346I 2015 08 13.59972 23 18 57.381 -14 03 07.78 22.9G 591392 F51 C~346I 2015 08 13.61245 23 18 57.325 -14 03 08.55 22.8G 591392 F51 C~346I 2015 10 18.36753 23 14 07.931 -14 31 33.35 22.7G 591392 F51 C~346I 2016 08 02.51896 23 25 22.928 -13 24 15.85 22.4G 591392 F51 C~346I 2016 08 02.53002 23 25 22.888 -13 24 16.16 22.5G 591392 F51 C~346I 2016 08 02.54107 23 25 22.853 -13 24 16.55 22.5G 591392 F51 C~346I 2016 08 02.55212 23 25 22.797 -13 24 16.95 22.4G 591392 F51 C~346I 2016 08 14.52100 23 24 38.594 -13 30 31.43 23.1G 591392 F51 C~346I 2016 08 14.52916 23 24 38.530 -13 30 31.52 21.8G 591392 F51 C~346I 2016 08 14.53251 23 24 38.521 -13 30 31.68 22.8G 591392 F51 C~346I 2016 08 14.54407 23 24 38.494 -13 30 31.81 22.5G 591392 F51 C~346I 2016 08 27.45942 23 23 43.344 -13 37 25.38 22.9G 591392 F51 C~346I 2016 08 27.47054 23 23 43.290 -13 37 25.62 22.0G 591392 F51 C~346I 2016 08 27.48166 23 23 43.251 -13 37 25.86 22.1G 591392 F51 C~346I 2016 08 27.49276 23 23 43.174 -13 37 26.05 22.3G 591392 F51 C~346I 2017 07 25.56455 23 31 30.802 -12 46 28.01 22.7G 591392 F51 C~346I 2017 07 25.57572 23 31 30.770 -12 46 28.38 22.6G 591392 F51 C~346I 2017 07 25.58688 23 31 30.737 -12 46 28.59 22.7G 591392 F51 C~346I 2017 07 25.59803 23 31 30.705 -12 46 28.99 23.2G 591392 F51 C~346I 2017 08 18.48938 23 30 08.587 -12 58 38.27 22.2G 591392 F51 C~346I 2017 08 18.50054 23 30 08.535 -12 58 38.70 22.3G 591392 F51 C~346I 2017 08 18.51169 23 30 08.492 -12 58 38.99 22.6G 591392 F51 C~346I 2017 08 18.52288 23 30 08.449 -12 58 39.37 22.7G 591392 F51 C~346I 2017 09 15.40657 23 28 03.089 -13 13 05.32 22.7G 591392 F51 C~346I 2017 09 15.41767 23 28 03.038 -13 13 05.48 22.2G 591392 F51 C~346I 2017 09 15.42887 23 28 02.988 -13 13 05.92 22.3G 591392 F51 C~346I 2017 09 15.43997 23 28 02.940 -13 13 06.11 22.5G 591392 F51 C~346I 2017 09 23.39475 23 27 25.845 -13 16 44.02 22.7G 591392 F51 C~346I 2017 09 23.40592 23 27 25.798 -13 16 44.43 22.3G 591392 F51 C~346I 2017 09 23.41704 23 27 25.744 -13 16 44.75 22.6G 591392 F51 C~346I 2017 09 23.42817 23 27 25.674 -13 16 45.08 22.9G 591392 F51 C~346I 2017 10 11.39774 23 26 07.093 -13 23 24.78 22.0G 591392 F51 C~346I 2017 11 07.29942 23 24 39.748 -13 28 00.72 22.6G 591392 F51 C~346I 2020 09 14.36382 23 45 10.305 -11 29 17.84 22.4w 591392 F51 C~48AU 2020 09 14.39111 23 45 10.176 -11 29 18.55 22.3w 591392 F51 C~48AU 2020 09 14.40491 23 45 10.101 -11 29 18.79 22.3w 591392 F51 C~48AU 2021 08 16.520140 23 52 48.940 -10 38 59.22 22.3w 591392 F51 C~4yQZ 2021 08 16.531356 23 52 48.920 -10 38 59.73 22.5w 591392 F51 C~4yQZ 2021 08 16.542608 23 52 48.861 -10 39 00.34 22.4w 591392 F51 C~4yQZ
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 -0.18 0.00 0.44
2 0.2346 0.00 -0.15 0.00 -0.03
3 1.1740 0.00 0.07 0.00 0.02
4 1.1741 0.00 0.07 0.00 -0.06
5 1.1741 0.00 -0.04 0.00 0.01
6 1.1741 0.00 0.06 0.00 -0.04
7 2.1488 0.00 -0.10 0.00 0.09
8 2.1489 0.00 0.15 0.00 -0.19
9 2.1489 0.00 -0.20 0.00 -0.05
10 2.1490 0.00 0.18 0.00 -0.29
11 3.1344 0.00 -0.05 0.00 -0.00
12 3.1344 0.00 0.07 0.00 -0.13
13 3.1344 0.00 0.02 0.00 0.14
14 3.1345 0.00 0.12 0.00 -0.02
15 3.1810 0.00 0.08 0.00 -0.34
16 3.1810 0.00 -0.53 0.00 0.14
17 3.1810 0.00 -0.04 0.00 -0.19
18 3.1811 0.00 0.23 0.00 -0.17
19 3.1919 0.00 -0.00 0.00 0.26
20 3.1973 0.00 -0.00 0.00 0.07
21 3.1973 0.00 0.02 0.00 0.07
22 3.1973 0.00 0.14 0.00 -0.05
23 3.1974 0.00 0.09 0.00 -0.06
24 3.2547 0.00 -0.11 0.00 0.24
25 3.2547 0.00 -0.01 0.00 -0.11
26 3.3419 0.00 0.50 0.00 0.20
27 3.3419 0.00 0.15 0.00 0.09
28 4.0082 0.00 0.21 0.00 0.17
29 4.1856 0.00 -0.20 0.00 0.07
30 4.1856 0.00 -0.05 0.00 0.01
31 4.1856 0.00 -0.64 0.00 -0.00
32 4.2404 0.00 -0.36 0.00 0.16
33 4.2405 0.00 0.20 0.00 -0.22
34 4.2405 0.00 -0.05 0.00 -0.21
35 4.2405 0.00 0.26 0.00 -0.36
36 4.2457 0.00 0.04 0.00 0.08
37 4.2458 0.00 0.02 0.00 0.10
38 4.2458 0.00 -0.21 0.00 -0.11
39 4.2458 0.00 0.11 0.00 -0.25
40 4.4206 0.00 -0.05 0.00 0.01
41 4.4260 0.00 0.18 0.00 0.02
42 5.1444 0.00 0.14 0.00 0.41
43 5.1444 0.00 0.08 0.00 0.04
44 5.3244 0.00 0.08 0.00 0.15
45 6.1161 0.00 0.13 0.00 -0.00
46 6.1161 0.00 0.10 0.00 0.02
47 6.1161 0.00 0.15 0.00 -0.03
48 6.1162 0.00 -0.12 0.00 -0.10
49 6.1489 0.00 0.23 0.00 -0.11
50 6.1490 0.00 -0.23 0.00 0.06
51 6.1490 0.00 -0.15 0.00 0.00
52 6.1490 0.00 0.15 0.00 0.24
53 6.1844 0.00 -0.05 0.00 -0.11
54 6.1844 0.00 -0.10 0.00 0.00
55 6.1844 0.00 0.08 0.00 0.11
56 6.1845 0.00 -0.31 0.00 0.28
57 7.0936 0.00 0.02 0.00 0.02
58 7.0936 0.00 0.00 0.00 -0.04
59 7.0937 0.00 -0.03 0.00 0.07
60 7.0937 0.00 -0.05 0.00 -0.02
61 7.1591 0.00 0.07 0.00 -0.01
62 7.1591 0.00 -0.01 0.00 -0.08
63 7.1592 0.00 0.04 0.00 -0.02
64 7.1592 0.00 0.10 0.00 -0.04
65 7.2356 0.00 0.02 0.00 0.05
66 7.2356 0.00 0.05 0.00 0.20
67 7.2356 0.00 0.10 0.00 0.08
68 7.2356 0.00 0.18 0.00 0.21
69 7.2574 0.00 -0.05 0.00 0.01
70 7.2575 0.00 0.04 0.00 -0.11
71 7.2575 0.00 0.01 0.00 -0.14
72 7.2575 0.00 -0.25 0.00 -0.18
73 7.3067 0.00 0.01 0.00 -0.42
74 7.3804 0.00 -0.07 0.00 0.00
75 10.2334 0.00 0.04 0.00 -0.15
76 10.2335 0.00 0.03 0.00 -0.04
77 10.2335 0.00 -0.12 0.00 0.13
78 11.1537 0.00 -0.14 0.00 0.24
79 11.1538 0.00 0.18 0.00 0.08
80 11.1538 0.00 -0.08 0.00 -0.18
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.
591392 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 45.740 45.740 45.740 ecceobj 0.142 0.142 0.142 incobj 8.889 8.889 8.889 qmin 38.673 38.673 38.673 qmax 52.880 52.881 52.882 amean 45.618 45.618 45.618 amin 45.231 45.243 45.232 amax 46.041 46.042 46.042 emean 0.135 0.135 0.135 emin 0.120 0.121 0.120 emax 0.149 0.149 0.149 imean 7.005 7.004 7.005 imin 6.501 6.501 6.501 imax 7.616 7.617 7.616 excite_mean 0.182 0.182 0.182 fracstop 1.000 1.000 1.000 cjmean 3.081 3.081 3.081 libcent 0 -180.0 -180.0 -180.0 libamp 0 -180.0 -180.0 -180.0 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 188.9 188.9 188.9 kozaiamp 180.0 179.9 180.0