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: 127546
# Created Tue Dec 24 02:06:50 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 95 observations of 96
# Arc: 21.42y
# First observation: 2002/12/04
# Last observation: 2024/05/04
# Chi-squared of fit: 940.69 DOF: 184 RMS: 0.56
# Min/Max residuals: -1.75 1.99
# Exact a, adot, b, bdot, g, gdot:
5.514251E-06 1.713991E-02 2.710507E-05 7.902844E-02 4.750570E-02 -1.544338E-02
# 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
0.701832 91.322340 0.327290 0.011324 -0.925139 2452612.870803
# Heliocentric elements and errors
Epoch: 2452612.5000 = 2002/12/04
Mean Anomaly: 356.24759 +/- 0.000
Argument of Peri: 27.91450 +/- 0.000
Long of Asc Node: 90.32716 +/- 0.000
Inclination: 77.84567 +/- 0.000
Eccentricity: 0.68881951 +/- 0.0000
Semi-Major Axis: 67.45043627 +/- 0.0000
Time of Perihelion: 2454721.5343 +/- 0.0
Perihelion: 20.98925956 +/- 0.0000
Aphelion: 113.91161299 +/- 0.0000
Period (y) 553.9689 +/- 0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -0.18116577 +/- 0.0000
Ecliptic Y 21.98031726 +/- 0.0000
Ecliptic Z 0.25841165 +/- 0.0000
Ecliptic XDOT -0.00097302 +/- 0.0000
Ecliptic YDOT -0.00097203 +/- 0.0000
Ecliptic ZDOT 0.00454353 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 21.98269277 +/- 0.0000
Geocenter to KBO 21.05024966 +/- 0.0000
# Hcoef: 8.09
The following table shows the complete astrometric record for 127546. 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 (127546) followed by the observatory code and reference code for the source of the astrometry.
2002 12 04.37006 06 05 47.74 +24 08 04.1 20.8R 127546 695 Ch0145 2002 12 04.47819 06 05 46.52 +24 08 09.3 127546 695 Ch0145 2002 12 05.36248 06 05 36.71 +24 08 50.7 127546 695 Ch0145 2003 01 03.19013 05 59 59.98 +24 30 46.3 21.0R 127546 688 Ch0145 2003 01 03.30213 05 59 58.69 +24 30 51.1 127546 688 Ch0145 2003 01 30.17579 05 55 17.82 +24 49 51.2 21.1R 127546 688 Ch1705 2003 01 30.25700 05 55 17.08 +24 49 54.6 127546 688 Ch1705 2003 03 01.78552 05 52 08.78 +25 09 56.9 21.2R 127546 230 Ch4226 2003 03 01.81881 05 52 08.69 +25 09 58.0 20.9R 127546 230 Ch4226 2003 03 06.15277 05 51 56.71 +25 12 44.5 21.1R 127546 662 Ch6164 2003 03 06.20488 05 51 56.60 +25 12 46.6 127546 662 Ch6164 2003 10 01.58522 06 17 32.78 +27 41 22.0 21.5R 127546 568 Ci6926 2003 10 02.52623 06 17 32.52 +27 42 15.1 127546 568 Ci6926 2003 10 02.56138 06 17 32.49 +27 42 16.7 127546 568 Ci6926 2003 11 20.45451 06 13 07.77 +28 29 43.0 20.2R 127546 695 Cj3701 2003 11 20.51402 06 13 07.20 +28 29 46.3 127546 695 Cj3701 2004 12 14.24993 06 13 46.82 +33 34 34.3 21.5R 127546 918 Cq3767 2004 12 14.32021 06 13 46.03 +33 34 38.8 21.1R 127546 918 Cq3767 2005 02 04.20299 06 03 16.01 +34 09 23.6 20.6R 127546 709 Cm6367 2005 02 04.23454 06 03 15.74 +34 09 24.8 20.8R 127546 709 Cm6760 2005 02 04.26611 06 03 15.40 +34 09 25.2 21.1R 127546 709 Cm6367 2005 02 04.29769 06 03 15.07 +34 09 25.1 21.3R 127546 709 Cm6367 2005 02 04.78452 06 03 10.57 +34 09 37.5 127546 621 Cm6760 2005 02 04.81962 06 03 10.29 +34 09 37.7 22. R 127546 621 Cm6760 2005 02 05.80454 06 03 01.32 +34 10 01.6 127546 621 Cm6760 2005 02 08.81069 06 02 35.21 +34 11 12.7 127546 621 Cm6760 2005 02 08.84776 06 02 34.88 +34 11 13.5 21. R 127546 621 Cm6760 2005 02 09.13905 06 02 32.52 +34 11 19.7 20.2R 127546 688 Cm6760 2005 02 09.25223 06 02 31.53 +34 11 22.4 127546 688 Cm6760 2005 02 14.17219 06 01 53.12 +34 13 08.5 21.0R 127546 709 Cm6760 2005 02 14.20377 06 01 52.87 +34 13 09.6 20.7R 127546 709 Cm6760 2006 01 28.17144 06 09 46.73 +38 53 41.2 21.2R 127546 688 Cq1751 2006 01 28.23847 06 09 45.98 +38 53 42.5 127546 688 Cq1751 2007 01 12.94521 06 19 25.150 +43 38 00.07 21.4V 127546 493 Cz7541 2007 01 12.99720 06 19 24.383 +43 38 01.91 21.4V 127546 493 Cz7541 2007 01 13.04167 06 19 23.728 +43 38 03.46 21.3V 127546 493 Cz7541 2007 01 13.09344 06 19 22.857 +43 38 06.92 20.2V 127546 493 Cz7541 2007 01 13.14465 06 19 22.226 +43 38 06.82 21.4V 127546 493 Cz7541 2007 01 13.17468 06 19 21.781 +43 38 07.85 21.3V 127546 493 Cz7541 2008 11 10.80999 06 52 32.20 +51 53 02.0 22.0R 127546 250 S~06HD 2008 11 10.81694 06 52 32.13 +51 53 02.8 127546 250 S~06HD 2008 11 10.82319 06 52 32.07 +51 53 03.6 127546 250 S~06HD 2008 11 10.83013 06 52 32.00 +51 53 04.4 127546 250 S~06HD 2011 01 08.48386 07 04 08.26 +62 43 16.2 21.0R 127546 695 C~0UMb 2011 01 08.49041 07 04 08.11 +62 43 16.3 127546 695 C~0UMb 2011 11 15.570115 07 41 50.702 +65 22 07.20 21.9G 127546 F51 C~43Z5 2011 11 15.578504 07 41 50.594 +65 22 08.12 21.4G 127546 F51 C~43Z5 2011 12 23.429365 07 30 59.020 +66 46 02.32 20.8G 127546 F51 C~43Z5 2012 10 28.581197 08 10 46.102 +68 28 56.09 21.2G 127546 F51 C~43Z5 2012 12 28.440649 07 57 10.333 +70 58 57.80 21.5G 127546 F51 C~43Z5 2012 12 28.455609 07 57 09.936 +70 58 59.62 20.9G 127546 F51 C~43Z5 2013 11 25.626257 08 48 02.354 +73 10 10.83 21.4G 127546 F51 C~43Z5 2013 11 25.628389 08 48 02.423 +73 10 11.01 20.9G 127546 F51 C~43Z5 2013 12 05.576121 08 46 13.296 +73 37 21.79 22.3G 127546 F51 C~43Z5 2014 01 21.508543 08 25 23.586 +75 10 18.93 21.1G 127546 F51 C~43Z5 2014 01 21.515174 08 25 23.391 +75 10 19.49 21.8G 127546 F51 C~43Z5 2014 03 13.308787 08 00 12.954 +75 07 01.29 22.0G 127546 F51 C~43Z5 2014 03 13.316055 08 00 12.816 +75 07 00.16 21.7G 127546 F51 C~43Z5 2014 03 13.316713 08 00 12.813 +75 06 59.81 21.8G 127546 F51 C~43Z5 2014 12 11.604799 09 41 47.070 +76 34 00.40 22.0G 127546 F51 C~43Z5 2014 12 11.633894 09 41 46.646 +76 34 05.27 21.7G 127546 F51 C~43Z5 2015 01 08.471742 09 32 35.302 +77 42 44.66 21.4G 127546 F51 C~43Z5 2015 01 08.474573 09 32 35.045 +77 42 45.23 21.7G 127546 F51 C~43Z5 2015 01 08.485164 09 32 34.787 +77 42 46.64 21.7G 127546 F51 C~43Z5 2015 01 08.498593 09 32 34.349 +77 42 48.47 22.0G 127546 F51 C~43Z5 2015 01 08.501421 09 32 34.216 +77 42 48.41 21.5G 127546 F51 C~43Z5 2015 01 08.511976 09 32 33.974 +77 42 49.98 21.3G 127546 F51 C~43Z5 2015 01 10.510934 09 31 33.142 +77 46 53.82 21.1G 127546 F51 C~43Z5 2015 02 25.362917 09 02 21.776 +78 31 20.49 21.1G 127546 F51 C~43Z5 2015 02 25.376753 09 02 21.300 +78 31 20.55 21.7G 127546 F51 C~43Z5 2015 02 25.390713 09 02 20.765 +78 31 20.75 21.0G 127546 F51 C~43Z5 2015 02 25.404155 09 02 20.351 +78 31 20.44 21.6G 127546 F51 C~43Z5 2016 01 25.531148 10 47 47.735 +79 56 32.98 22.0G 127546 F51 C~43Z5 2016 03 17.307347 10 12 19.009 +80 35 34.19 21.3G 127546 F51 C~43Z5 2017 05 21.273197 11 25 19.684 +79 59 49.17 21.8G 127546 F51 C~43Z5 2017 05 21.285651 11 25 19.577 +79 59 47.46 22.0G 127546 F51 C~43Z5 2017 05 21.298110 11 25 19.549 +79 59 45.76 21.8G 127546 F51 C~43Z5 2017 05 21.310603 11 25 19.482 +79 59 44.27 22.3G 127546 F51 C~43Z5 2017 06 08.256359 11 26 24.987 +79 19 16.78 20.9G 127546 F51 C~43Z5 2018 03 08.499932 13 37 12.596 +79 54 58.33 22.2G 127546 F51 C~43Z6 2018 05 19.145220 12 54 23.22 +79 34 48.7 21.8G 127546 705 C~2rO0 2018 05 19.181180 12 54 22.39 +79 34 44.9 21.9G 127546 705 C~2rO0 2018 05 19.209220 12 54 21.71 +79 34 41.8 21.9G 127546 705 C~2rO0 2018 07 08.283867 12 50 20.254 +77 38 29.50 21.6G 127546 F51 C~43Z6 2018 07 08.297700 12 50 20.397 +77 38 27.30 21.8G 127546 F51 C~43Z6 2018 07 08.311506 12 50 20.615 +77 38 25.23 22.3G 127546 F51 C~43Z6 2018 07 08.325296 12 50 20.699 +77 38 23.48 21.3G 127546 F51 C~43Z6 2019 04 15.432530 14 23 07.890 +78 12 36.79 22.0G 127546 F51 C~43Z6 2019 04 15.442651 14 23 07.577 +78 12 36.74 22.0G 127546 F51 C~43Z6 2020 06 29.311348 14 36 33.221 +74 18 43.32 22.1G 127546 F51 C~43Z6 2020 06 29.320498 14 36 33.128 +74 18 42.08 22.5G 127546 F51 C~43Z6 2020 06 29.329670 14 36 33.014 +74 18 40.83 22.4G 127546 F51 C~43Z6 2020 06 29.338826 14 36 32.960 +74 18 39.53 22.1G 127546 F51 C~43Z6 2024 05 04.370310 16 19 42.759 +64 25 45.61 22.5G 127546 G37 C~8343 2024 05 04.405090 16 19 42.179 +64 25 46.40 127546 G37 C~8343 2024 05 04.439700 16 19 41.606 +64 25 47.42 127546 G37 C~8343
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 0.04 0.00 -0.17
2 0.0003 0.00 -0.04 0.00 0.01
3 0.0027 0.00 0.13 0.00 -0.02
4 0.0816 0.00 0.12 0.00 0.11
5 0.0819 0.00 0.52 0.00 -0.05
6 0.1555 0.00 0.06 0.00 -0.18
7 0.1557 0.00 -0.07 0.00 -0.09
8 0.2393 0.00 -0.06 0.00 -0.24
9 0.2394 0.00 0.26 0.00 -0.41
10 0.2513 0.00 -0.27 0.00 0.39
11 0.2514 0.00 -0.01 0.00 0.52
12 0.8247 0.00 0.04 0.00 -0.18
13 0.8273 0.00 0.27 0.00 -0.07
14 0.8274 0.00 0.10 0.00 -0.48
15 0.9612 0.00 -0.04 0.00 -0.04
16 0.9614 0.00 0.37 0.00 -0.12
17 2.0284 0.00 -0.69 0.00 0.28
18 2.0286 0.00 1.28 0.00 0.80
19 2.1707 0.00 0.97 0.00 0.30
20 2.1707 0.00 1.38 0.00 0.72
21 2.1708 0.00 0.74 0.00 0.36
22 2.1709 0.00 0.24 0.00 -0.50
23 2.1723 0.00 -0.52 0.00 -0.03
24 2.1723 0.00 0.16 0.00 -0.70
25 2.1750 0.00 -0.56 0.00 -0.75
26 2.1833 0.00 -0.53 0.00 0.03
27 2.1834 0.00 -0.74 0.00 -0.02
28 2.1842 0.00 0.29 0.00 -0.52
29 2.1845 0.00 -0.14 0.00 -0.36
30 2.1980 0.00 0.46 0.00 -0.04
31 2.1980 0.00 0.26 0.00 0.43
32 3.1507 0.00 -0.25 0.00 0.12
33 3.1509 0.00 0.14 0.00 -0.11
34 4.1084 0.00 -1.02 0.00 0.10
35 4.1085 0.00 -1.03 0.00 0.15
36 4.1086 0.00 -1.04 0.00 0.18
37 4.1088 0.00 ( -2.71) 0.00 ( 1.90)
38 4.1089 0.00 -0.93 0.00 0.10
39 4.1090 0.00 -1.04 0.00 0.14
40 5.9369 0.00 -0.21 0.00 0.67
41 5.9369 0.00 -0.26 0.00 0.62
42 5.9369 0.00 -0.26 0.00 0.66
43 5.9369 0.00 -0.31 0.00 0.61
44 8.0961 0.00 0.48 0.00 -0.11
45 8.0962 0.00 0.48 0.00 -0.35
46 8.9478 0.00 0.56 0.00 0.21
47 8.9479 0.00 0.18 0.00 -0.17
48 9.0515 0.00 -0.07 0.00 -0.11
49 9.9006 0.00 -0.27 0.00 -0.20
50 10.0673 0.00 0.17 0.00 -0.20
51 10.0673 0.00 0.37 0.00 0.05
52 10.9767 0.00 -0.92 0.00 -0.03
53 10.9768 0.00 0.38 0.00 -0.21
54 11.0040 0.00 -1.08 0.00 -0.20
55 11.1325 0.00 -0.54 0.00 -0.09
56 11.1325 0.00 0.06 0.00 0.05
57 11.2716 0.00 -1.23 0.00 0.53
58 11.2716 0.00 -1.27 0.00 -0.15
59 11.2716 0.00 -1.13 0.00 -0.46
60 12.0198 0.00 1.22 0.00 -0.02
61 12.0199 0.00 -0.82 0.00 0.05
62 12.0961 0.00 1.70 0.00 -0.28
63 12.0961 0.00 -0.87 0.00 -0.06
64 12.0961 0.00 0.10 0.00 0.03
65 12.0962 0.00 -0.33 0.00 0.18
66 12.0962 0.00 -1.03 0.00 -0.23
67 12.0962 0.00 0.17 0.00 0.02
68 12.1017 0.00 -0.85 0.00 -0.10
69 12.2272 0.00 -1.58 0.00 -0.27
70 12.2273 0.00 -0.81 0.00 -0.11
71 12.2273 0.00 -0.85 0.00 0.19
72 12.2273 0.00 0.62 0.00 -0.01
73 13.1421 0.00 -1.75 0.00 0.25
74 13.2839 0.00 0.86 0.00 -0.16
75 14.4611 0.00 0.68 0.00 0.03
76 14.4611 0.00 -0.04 0.00 -0.08
77 14.4611 0.00 0.43 0.00 -0.17
78 14.4612 0.00 0.30 0.00 -0.05
79 14.5103 0.00 1.33 0.00 -0.12
80 15.2584 0.00 -0.50 0.00 -0.07
81 15.4546 0.00 -0.37 0.00 -0.11
82 15.4547 0.00 0.33 0.00 -0.05
83 15.4547 0.00 0.37 0.00 -0.12
84 15.5918 0.00 1.67 0.00 -0.27
85 15.5919 0.00 1.27 0.00 -0.31
86 15.5919 0.00 1.99 0.00 -0.22
87 15.5919 0.00 0.68 0.00 0.19
88 16.3616 0.00 -0.23 0.00 -0.24
89 16.3616 0.00 0.48 0.00 -0.40
90 17.5686 0.00 -0.41 0.00 -0.02
91 17.5687 0.00 -0.09 0.00 0.02
92 17.5687 0.00 -0.09 0.00 0.05
93 17.5687 0.00 0.81 0.00 0.03
94 21.4155 0.00 -0.23 0.00 0.23
95 21.4156 0.00 -0.18 0.00 0.10
96 21.4157 0.00 -0.07 0.00 0.22
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.
127546 quality flag:3 Type: CENTAURR CENTAURR CENTAURR axisobj 67.107 67.106 67.108 ecceobj 0.687 0.687 0.687 incobj 77.869 77.869 77.869 qmin 15.713 15.322 16.085 qmax 121.511 119.123 120.592 amean 66.881 66.309 66.805 amin 65.058 63.499 65.693 amax 69.081 68.472 68.901 emean 0.698 0.701 0.697 emin 0.669 0.669 0.669 emax 0.763 0.767 0.761 imean 76.152 76.059 76.124 imin 74.575 74.407 74.369 imax 77.151 77.113 77.159 excite_mean 1.196 1.197 1.195 fracstop 0.486 0.504 0.476 cjmean 0.963 0.965 0.964 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 239.9 241.2 241.5 kozaiamp 180.0 180.0 180.0