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: 555591
# Created Fri Nov 22 02:07:33 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 99 observations of 99
# Arc: 11.02y
# First observation: 2012/02/13
# Last observation: 2023/02/20
# Chi-squared of fit: 158.87 DOF: 192 RMS: 0.22
# Min/Max residuals: -1.14 0.92
# Exact a, adot, b, bdot, g, gdot:
1.700777E-05 3.089679E-02 -7.717161E-06 -1.563057E-02 2.937611E-02 6.748946E-05
# 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
8.642808 124.497735 -0.329885 0.140103 -0.921594 2455970.803436
# Heliocentric elements and errors
Epoch: 2455970.5000 = 2012/02/13
Mean Anomaly: 2.57986 +/- 0.000
Argument of Peri: 157.65236 +/- 0.000
Long of Asc Node: 321.11423 +/- 0.000
Inclination: 28.10730 +/- 0.000
Eccentricity: 0.23215651 +/- 0.0000
Semi-Major Axis: 45.51192304 +/- 0.0000
Time of Perihelion: 2455166.8264 +/- 0.0
Perihelion: 34.94603393 +/- 0.0000
Aphelion: 56.07781214 +/- 0.0000
Period (y) 307.0407 +/- 0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -19.85842455 +/- 0.0000
Ecliptic Y 28.31912345 +/- 0.0000
Ecliptic Z 5.11524252 +/- 0.0000
Ecliptic XDOT -0.00250533 +/- 0.0000
Ecliptic YDOT -0.00144111 +/- 0.0000
Ecliptic ZDOT -0.00143918 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 34.96419405 +/- 0.0000
Geocenter to KBO 34.04129954 +/- 0.0000
# Hcoef: 7.39
The following table shows the complete astrometric record for 555591. 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 (555591) followed by the observatory code and reference code for the source of the astrometry.
2012 02 13.30267 08 36 36.019 +27 30 53.47 23.1G 555591 F51 C~346M 2012 02 13.31719 08 36 35.938 +27 30 53.64 23.3G 555591 F51 C~346M 2012 02 13.33173 08 36 35.840 +27 30 53.90 22.8G 555591 F51 C~346M 2012 02 13.34632 08 36 35.750 +27 30 54.09 22.4G 555591 F51 C~346M 2013 02 12.28538 08 43 15.053 +26 11 17.04 23.0G 555591 F51 C~346M 2013 02 12.29856 08 43 15.017 +26 11 17.52 23.0G 555591 F51 C~346M 2013 02 12.31178 08 43 14.920 +26 11 17.48 22.5G 555591 F51 C~346M 2013 02 12.32499 08 43 14.838 +26 11 17.51 23.2G 555591 F51 C~346M 2013 05 09.28563 08 39 35.824 +25 55 55.52 22.5G 555591 F51 C~346M 2013 05 09.28959 08 39 35.822 +25 55 55.87 22.5G 555591 F51 C~346M 2013 05 09.29354 08 39 35.869 +25 55 54.98 22.5G 555591 F51 C~346M 2013 05 09.29749 08 39 35.873 +25 55 55.25 22.9G 555591 F51 C~346M 2014 01 01.43679 08 54 03.330 +24 39 24.11 22.3G 555591 F51 C~346M 2014 01 01.45077 08 54 03.254 +24 39 24.23 22.2G 555591 F51 C~346M 2014 03 02.24159 08 48 00.473 +24 52 54.97 22.7G 555591 F51 C~346M 2014 05 17.29357 08 46 13.162 +24 34 41.33 21.9G 555591 F51 C~346M 2014 10 28.61608 09 02 24.210 +23 08 34.30 23.4G 555591 F51 C~346M 2014 12 21.59488 09 01 11.637 +23 14 19.20 22.8G 555591 F51 C~346M 2014 12 21.60850 09 01 11.594 +23 14 19.05 23.1G 555591 F51 C~346M 2014 12 21.62221 09 01 11.530 +23 14 19.43 22.5G 555591 F51 C~346M 2014 12 21.63606 09 01 11.448 +23 14 19.71 22.9G 555591 F51 C~346M 2014 12 26.46152 09 00 49.520 +23 15 39.18 24.0G 555591 F51 C~346M 2015 01 14.38110 08 59 07.094 +23 21 14.85 22.6G 555591 F51 C~346M 2015 01 14.39335 08 59 07.033 +23 21 15.09 22.9G 555591 F51 C~346M 2015 01 14.40558 08 59 06.962 +23 21 15.28 22.8G 555591 F51 C~346M 2015 01 14.41785 08 59 06.874 +23 21 15.45 23.4G 555591 F51 C~346M 2015 01 16.53623 08 58 54.152 +23 21 53.67 23.0G 555591 F51 C~346M 2015 01 16.54848 08 58 54.087 +23 21 54.02 22.8G 555591 F51 C~346M 2015 01 16.56077 08 58 53.994 +23 21 54.21 22.8G 555591 F51 C~346M 2015 01 16.57307 08 58 53.919 +23 21 54.45 23.2G 555591 F51 C~346M 2015 01 20.37178 08 58 30.698 +23 23 02.04 23.0G 555591 F51 C~346M 2015 01 20.38381 08 58 30.624 +23 23 02.15 22.3G 555591 F51 C~346M 2015 01 20.39585 08 58 30.564 +23 23 02.63 22.2G 555591 F51 C~346M 2015 01 20.40809 08 58 30.483 +23 23 02.77 22.5G 555591 F51 C~346M 2015 01 22.39273 08 58 18.157 +23 23 37.76 22.3G 555591 F51 C~346M 2015 01 22.40486 08 58 18.087 +23 23 38.15 22.3G 555591 F51 C~346M 2015 01 22.41699 08 58 18.009 +23 23 38.15 22.8G 555591 F51 C~346M 2015 01 22.42913 08 58 17.928 +23 23 38.30 23.5G 555591 F51 C~346M 2015 03 16.38614 08 53 13.039 +23 32 36.59 22.7G 555591 F51 C~346M 2015 03 16.39835 08 53 12.994 +23 32 36.87 22.9G 555591 F51 C~346M 2015 03 16.41058 08 53 12.933 +23 32 36.87 22.2G 555591 F51 C~346M 2015 04 10.30224 08 51 58.808 +23 29 54.10 23.5G 555591 F51 C~346M 2015 04 10.31404 08 51 58.772 +23 29 54.06 23.2G 555591 F51 C~346M 2015 04 10.32582 08 51 58.771 +23 29 53.83 23.9G 555591 F51 C~346M 2015 04 10.33765 08 51 58.698 +23 29 53.63 22.9G 555591 F51 C~346M 2016 01 08.42455 09 05 50.726 +21 56 42.69 22.2G 555591 F51 C~346M 2016 01 08.42733 09 05 50.706 +21 56 42.78 22.6G 555591 F51 C~346M 2016 01 08.43904 09 05 50.656 +21 56 42.50 23.0G 555591 F51 C~346M 2016 01 08.44184 09 05 50.627 +21 56 42.93 22.6G 555591 F51 C~346M 2016 01 08.45359 09 05 50.571 +21 56 43.12 22.2G 555591 F51 C~346M 2016 01 08.45642 09 05 50.545 +21 56 43.09 22.7G 555591 F51 C~346M 2016 01 08.46816 09 05 50.505 +21 56 43.19 22.3G 555591 F51 C~346M 2016 01 31.36118 09 03 33.569 +22 03 30.88 23.1G 555591 F51 C~346M 2016 01 31.37610 09 03 33.473 +22 03 31.53 22.3G 555591 F51 C~346M 2016 01 31.39092 09 03 33.379 +22 03 31.70 22.5G 555591 F51 C~346M 2016 01 31.40575 09 03 33.271 +22 03 32.35 22.4G 555591 F51 C~346M 2016 02 03.39921 09 03 14.502 +22 04 22.04 20.7G 555591 F51 C~346M 2016 02 05.54822 09 03 00.995 +22 04 56.75 22.8G 555591 F51 C~346M 2016 02 05.56070 09 03 00.929 +22 04 57.13 22.9G 555591 F51 C~346M 2016 02 05.57319 09 03 00.829 +22 04 56.96 23.5G 555591 F51 C~346M 2016 02 11.28636 09 02 25.168 +22 06 24.70 22.0G 555591 F51 C~346M 2016 02 11.29830 09 02 25.106 +22 06 24.90 22.2G 555591 F51 C~346M 2016 02 11.30994 09 02 25.042 +22 06 25.08 22.5G 555591 F51 C~346M 2016 02 11.32158 09 02 24.986 +22 06 25.32 22.2G 555591 F51 C~346M 2016 02 27.47974 09 00 49.104 +22 09 42.14 21.4G 555591 F51 C~346M 2016 03 03.28211 09 00 23.067 +22 10 21.25 22.5G 555591 F51 C~346M 2016 03 03.29595 09 00 22.962 +22 10 21.67 23.1G 555591 F51 C~346M 2016 03 03.30913 09 00 22.877 +22 10 21.87 22.2G 555591 F51 C~346M 2016 03 03.32233 09 00 22.785 +22 10 21.92 23.2G 555591 F51 C~346M 2016 03 14.25208 08 59 29.438 +22 11 17.15 21.6G 555591 F51 C~346M 2016 04 22.31245 08 57 52.659 +22 06 47.51 23.0G 555591 F51 C~346M 2016 04 28.27540 08 57 53.063 +22 05 00.36 22.6G 555591 F51 C~346M 2016 04 28.28801 08 57 53.057 +22 05 00.25 23.3G 555591 F51 C~346M 2016 04 28.30063 08 57 53.089 +22 05 00.28 22.8G 555591 F51 C~346M 2017 01 28.37868 09 09 49.355 +20 39 42.38 22.6G 555591 F51 C~346M 2017 01 28.39103 09 09 49.201 +20 39 42.32 21.5G 555591 F51 C~346M 2017 01 28.40322 09 09 49.193 +20 39 42.53 21.7G 555591 F51 C~346M 2017 02 04.51929 09 09 05.120 +20 41 46.89 22.4G 555591 F51 C~346M 2017 02 04.53182 09 09 05.069 +20 41 46.63 22.4G 555591 F51 C~346M 2017 02 04.54433 09 09 04.941 +20 41 47.60 21.8G 555591 F51 C~346M 2017 02 04.55685 09 09 04.908 +20 41 47.44 22.6G 555591 F51 C~346M 2018 01 14.55324 09 17 05.576 +19 11 44.83 22.6G 555591 F51 C~346M 2018 01 14.56558 09 17 05.491 +19 11 45.07 22.7G 555591 F51 C~346M 2018 01 14.57790 09 17 05.427 +19 11 45.30 22.5G 555591 F51 C~346M 2018 01 14.59025 09 17 05.356 +19 11 45.54 22.5G 555591 F51 C~346M 2018 01 15.56397 09 16 59.912 +19 12 03.24 22.2G 555591 F51 C~346M 2018 02 12.35055 09 14 13.182 +19 20 21.39 23.0G 555591 F51 C~346M 2018 02 12.36380 09 14 13.123 +19 20 21.86 22.5G 555591 F51 C~346M 2018 02 12.37711 09 14 13.023 +19 20 22.04 22.2G 555591 F51 C~346M 2018 02 12.39065 09 14 12.953 +19 20 22.39 22.7G 555591 F51 C~346M 2018 03 08.26638 09 11 57.509 +19 25 44.77 22.6G 555591 F51 C~346M 2018 03 08.27954 09 11 57.450 +19 25 44.76 22.2G 555591 F51 C~346M 2018 03 08.29273 09 11 57.369 +19 25 45.24 22.2G 555591 F51 C~346M 2018 03 08.30598 09 11 57.327 +19 25 45.12 22.4G 555591 F51 C~346M 2021 03 20.147230 09 28 00.688 +15 17 33.20 22.8G 555591 G37 C~4i0s 2021 03 20.187650 09 28 00.501 +15 17 33.63 555591 G37 C~4i0s 2021 03 20.226850 09 28 00.327 +15 17 34.10 555591 G37 C~4i0s 2023 02 20.244840 09 41 19.130 +12 21 27.22 22.7G 555591 G37 C~6IlX 2023 02 20.347460 09 41 18.548 +12 21 29.21 555591 G37 C~6IlX
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 -0.13 0.00 -0.12
2 0.0000 0.00 0.05 0.00 -0.06
3 0.0001 0.00 -0.04 0.00 0.08
4 0.0001 0.00 0.01 0.00 0.16
5 0.9993 0.00 -0.56 0.00 -0.16
6 0.9993 0.00 0.16 0.00 0.19
7 0.9993 0.00 -0.04 0.00 0.02
8 0.9994 0.00 -0.01 0.00 -0.08
9 1.2347 0.00 -0.27 0.00 0.15
10 1.2347 0.00 -0.43 0.00 0.62
11 1.2347 0.00 0.14 0.00 -0.15
12 1.2348 0.00 0.07 0.00 0.24
13 1.8840 0.00 0.07 0.00 -0.03
14 1.8840 0.00 0.08 0.00 -0.16
15 2.0477 0.00 0.39 0.00 -0.46
16 2.2560 0.00 -0.11 0.00 -0.38
17 2.7059 0.00 -0.16 0.00 -0.01
18 2.8536 0.00 0.04 0.00 0.10
19 2.8537 0.00 0.30 0.00 -0.26
20 2.8537 0.00 0.26 0.00 -0.10
21 2.8538 0.00 -0.05 0.00 -0.03
22 2.8670 0.00 -0.27 0.00 0.27
23 2.9188 0.00 -0.19 0.00 -0.02
24 2.9188 0.00 0.01 0.00 -0.00
25 2.9188 0.00 0.05 0.00 -0.04
26 2.9189 0.00 -0.15 0.00 -0.09
27 2.9247 0.00 -0.00 0.00 -0.07
28 2.9247 0.00 0.15 0.00 0.06
29 2.9247 0.00 -0.11 0.00 0.03
30 2.9248 0.00 -0.10 0.00 0.05
31 2.9352 0.00 -0.17 0.00 -0.13
32 2.9352 0.00 -0.15 0.00 -0.24
33 2.9352 0.00 0.08 0.00 0.02
34 2.9353 0.00 0.02 0.00 -0.06
35 2.9407 0.00 -0.09 0.00 0.06
36 2.9407 0.00 0.02 0.00 0.24
37 2.9408 0.00 -0.00 0.00 0.02
38 2.9408 0.00 -0.06 0.00 -0.04
39 3.0858 0.00 -0.11 0.00 -0.29
40 3.0858 0.00 0.01 0.00 0.00
41 3.0859 0.00 -0.10 0.00 0.01
42 3.1540 0.00 0.54 0.00 -0.07
43 3.1540 0.00 0.30 0.00 0.04
44 3.1541 0.00 0.59 0.00 -0.04
45 3.1541 0.00 -0.20 0.00 -0.08
46 3.9018 0.00 -0.06 0.00 0.21
47 3.9018 0.00 -0.12 0.00 0.24
48 3.9018 0.00 0.11 0.00 -0.25
49 3.9018 0.00 -0.09 0.00 0.13
50 3.9019 0.00 0.05 0.00 0.11
51 3.9019 0.00 -0.10 0.00 0.03
52 3.9019 0.00 0.29 0.00 -0.08
53 3.9646 0.00 0.27 0.00 -0.51
54 3.9646 0.00 0.26 0.00 -0.12
55 3.9646 0.00 0.26 0.00 -0.20
56 3.9647 0.00 0.06 0.00 0.19
57 3.9729 0.00 0.23 0.00 0.01
58 3.9788 0.00 0.15 0.00 -0.04
59 3.9788 0.00 0.34 0.00 0.14
60 3.9788 0.00 0.03 0.00 -0.22
61 3.9945 0.00 -0.41 0.00 0.02
62 3.9945 0.00 -0.22 0.00 0.04
63 3.9945 0.00 -0.08 0.00 0.05
64 3.9946 0.00 0.18 0.00 0.11
65 4.0388 0.00 0.08 0.00 0.92
66 4.0520 0.00 0.63 0.00 -0.35
67 4.0520 0.00 0.18 0.00 -0.04
68 4.0520 0.00 -0.03 0.00 0.06
69 4.0521 0.00 -0.35 0.00 0.01
70 4.0820 0.00 0.22 0.00 -0.13
71 4.1889 0.00 -0.38 0.00 0.06
72 4.2053 0.00 0.08 0.00 0.05
73 4.2053 0.00 -0.07 0.00 0.19
74 4.2053 0.00 0.35 0.00 0.47
75 4.9585 0.00 0.02 0.00 0.23
76 4.9585 0.00 -1.14 0.00 -0.06
77 4.9585 0.00 -0.11 0.00 -0.07
78 4.9780 0.00 -0.26 0.00 0.08
79 4.9780 0.00 0.16 0.00 -0.39
80 4.9781 0.00 -0.58 0.00 0.38
81 4.9781 0.00 0.10 0.00 0.01
82 5.9199 0.00 0.20 0.00 -0.12
83 5.9200 0.00 -0.02 0.00 -0.10
84 5.9200 0.00 0.07 0.00 -0.09
85 5.9200 0.00 0.05 0.00 -0.07
86 5.9227 0.00 0.16 0.00 0.21
87 5.9988 0.00 -0.24 0.00 -0.26
88 5.9988 0.00 0.11 0.00 -0.01
89 5.9988 0.00 -0.16 0.00 -0.05
90 5.9989 0.00 0.05 0.00 0.07
91 6.0642 0.00 -0.30 0.00 0.01
92 6.0643 0.00 -0.17 0.00 -0.13
93 6.0643 0.00 -0.36 0.00 0.22
94 6.0643 0.00 0.04 0.00 -0.03
95 9.0975 0.00 0.04 0.00 0.00
96 9.0976 0.00 -0.07 0.00 -0.01
97 9.0977 0.00 -0.07 0.00 0.03
98 11.0197 0.00 0.03 0.00 0.03
99 11.0200 0.00 0.31 0.00 -0.05
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.
555591 quality flag:3 Type: SCATEXTD SCATEXTD SCATEXTD axisobj 45.606 45.606 45.606 ecceobj 0.233 0.233 0.233 incobj 28.117 28.117 28.117 qmin 33.572 33.572 33.572 qmax 57.637 57.638 57.636 amean 45.374 45.374 45.374 amin 44.969 44.982 44.977 amax 45.847 45.846 45.872 emean 0.237 0.237 0.237 emin 0.216 0.216 0.216 emax 0.258 0.258 0.258 imean 29.175 29.177 29.176 imin 28.588 28.592 28.578 imax 29.726 29.712 29.724 excite_mean 0.542 0.542 0.542 fracstop 1.000 1.000 1.000 cjmean 2.745 2.745 2.745 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 190.2 190.1 190.1 kozaiamp 180.0 180.0 180.0