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: 24OR # Created Sun Nov 24 02:11:16 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 117 observations of 117 # Arc: 13.66y # First observation: 2011/02/04 # Last observation: 2024/10/04 # Chi-squared of fit: 151.84 DOF: 228 RMS: 0.20 # Min/Max residuals: -1.21 1.45 # Exact a, adot, b, bdot, g, gdot: 2.109186E-05 6.260906E-02 5.514295E-07 2.692654E-03 4.695221E-02 -3.553143E-02 # Covariance matrix: 1.2971E-02 5.6341E-02 -2.4909E-03 3.2763E-03 5.7527E-05 8.8981E-03 5.6341E-02 4.1739E-01 -1.0820E-02 2.3293E-02 2.4989E-04 6.5299E-02 -2.4909E-03 -1.0820E-02 4.7837E-04 -6.2919E-04 -1.1048E-05 -1.7088E-03 3.2763E-03 2.3293E-02 -6.2919E-04 1.3189E-03 1.4531E-05 3.6463E-03 5.7527E-05 2.4989E-04 -1.1048E-05 1.4531E-05 2.5515E-07 3.9465E-05 8.8981E-03 6.5299E-02 -1.7088E-03 3.6463E-03 3.9465E-05 1.0218E-02 # lat0 lon0 xBary yBary zBary JD0 -25.948649 -140.172629 0.984936 -0.039560 -0.081359 2455596.768240 # Heliocentric elements and errors Epoch: 2455596.5000 = 2011/02/04 Mean Anomaly: 327.50395 +/- 0.005 Argument of Peri: 11.44764 +/- 0.001 Long of Asc Node: 303.92175 +/- 0.001 Inclination: 25.84729 +/- 0.004 Eccentricity: 0.58169465 +/- 0.0000 Semi-Major Axis: 29.47818129 +/- 0.0000 Time of Perihelion: 2460873.3836 +/- 0.9 Perihelion: 12.33088086 +/- 0.0000 Aphelion: 46.62548173 +/- 0.0000 Period (y) 160.0513 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -15.40349755 +/- 0.0000 Ecliptic Y -11.56821399 +/- 0.0000 Ecliptic Z -9.31941145 +/- 0.0000 Ecliptic XDOT 0.00371514 +/- 0.0000 Ecliptic YDOT -0.00164846 +/- 0.0000 Ecliptic ZDOT 0.00104778 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 21.39987050 +/- 0.0000 Geocenter to KBO 21.29852414 +/- 0.0000 # Hcoef: 8.77
The following table shows the complete astrometric record for 24OR. 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 (24OR) followed by the observatory code and reference code for the source of the astrometry.
2011 02 04.267474 13 48 39.09 -39 05 24.3 24OR 807 C~89YB 2014 06 23.023097 14 31 33.47 -42 10 04.7 21.2r 24OR W84 C~89YB 2014 06 23.136075 14 31 32.71 -42 09 54.2 21.3r 24OR W84 C~89YB 2014 06 27.004955 14 31 09.41 -42 03 55.9 21.0r 24OR W84 C~89YB 2015 03 03.301764 15 16 52.79 -43 42 41.5 21.3r 24OR W84 C~89YB 2015 03 03.303815 15 16 52.79 -43 42 41.7 21.3r 24OR W84 C~89YB 2015 05 28.199023 15 02 20.95 -43 46 35.9 20.9i 24OR W84 C~89YB 2015 05 28.206620 15 02 20.84 -43 46 35.2 24OR W84 C~89YB 2015 05 28.209616 15 02 20.81 -43 46 35.1 20.8z 24OR W84 C~89YB 2015 05 28.211669 15 02 20.76 -43 46 35.0 20.5Y 24OR W84 C~89YB 2017 04 28.251517 16 13 49.36 -44 40 28.9 21.0r 24OR W84 C~89YB 2017 04 28.252582 16 13 49.34 -44 40 28.9 21.4g 24OR W84 C~89YB 2017 05 05.409901 16 12 15.09 -44 40 34.3 19.4Y 24OR W84 C~89YB 2017 05 05.410579 16 12 15.09 -44 40 34.2 19.5z 24OR W84 C~89YB 2017 05 05.411270 16 12 15.08 -44 40 34.1 19.9i 24OR W84 C~89YB 2017 05 05.411949 16 12 15.06 -44 40 34.0 20.7r 24OR W84 C~89YB 2017 05 05.413003 16 12 15.04 -44 40 33.9 21.1g 24OR W84 C~89YB 2018 08 02.983915 16 30 54.79 -42 34 47.7 24OR W84 C~89YB 2019 05 02.234729 17 29 46.32 -42 22 09.1 21.1g 24OR W84 C~89YB 2019 05 02.235791 17 29 46.31 -42 22 09.2 20.9r 24OR W84 C~89YB 2019 05 03.315136 17 29 35.40 -42 22 36.1 24OR W84 C~89YB 2019 07 19.083178 17 11 24.32 -41 42 39.1 19.9z 24OR W84 C~89YB 2019 07 19.083857 17 11 24.29 -41 42 39.2 20.0i 24OR W84 C~89YB 2021 06 01.431652 18 45 53.24 -36 06 32.7 24OR W84 C~89YB 2021 07 16.976665 18 34 16.98 -35 53 54.9 24OR W84 C~89YB 2021 07 17.006779 18 34 16.52 -35 53 53.6 24OR W84 C~89YB 2021 09 24.999726 18 26 49.97 -34 29 10.1 24OR W84 C~89YB 2022 07 02.344404 19 19 12.36 -31 11 26.6 24OR W84 C~89YB 2022 07 04.443259 19 18 39.593 -31 11 06.74 19.5G 24OR F52 C~89YB 2022 07 04.451578 19 18 39.460 -31 11 06.72 19.4G 24OR F52 C~89YB 2022 07 04.459897 19 18 39.328 -31 11 06.59 19.4G 24OR F52 C~89YB 2022 07 04.468183 19 18 39.185 -31 11 06.51 19.6G 24OR F52 C~89YB 2022 08 01.337834 19 11 31.810 -31 00 17.88 19.8G 24OR F52 C~89YB 2022 08 01.346070 19 11 31.691 -31 00 17.61 19.8G 24OR F52 C~89YB 2022 08 01.354335 19 11 31.572 -31 00 17.29 19.9G 24OR F52 C~89YB 2022 08 01.362623 19 11 31.451 -31 00 16.98 19.9G 24OR F52 C~89YB 2022 08 16.156583 19 08 24.80 -30 49 32.1 20.2i 24OR W84 C~89YB 2022 09 15.085480 19 05 05.51 -30 18 30.1 20.8g 24OR W84 C~89YB 2023 05 16.566832 20 05 47.136 -25 15 51.55 19.5G 24OR F51 C~89YB 2023 05 16.577443 20 05 47.122 -25 15 51.32 19.8G 24OR F51 C~89YB 2023 05 16.590672 20 05 47.080 -25 15 51.20 19.9G 24OR F51 C~89YB 2023 06 16.529114 20 01 56.172 -25 12 38.74 19.9G 24OR F51 C~89YB 2023 06 20.484556 20 01 08.879 -25 12 36.91 19.6G 24OR F52 C~89YB 2023 06 28.481266 19 59 24.165 -25 12 34.87 19.6G 24OR F51 C~89YB 2023 06 28.490921 19 59 24.026 -25 12 34.99 19.5G 24OR F51 C~89YB 2023 06 28.500562 19 59 23.892 -25 12 34.92 19.6G 24OR F51 C~89YB 2023 06 28.510203 19 59 23.757 -25 12 34.90 19.6G 24OR F51 C~89YB 2023 08 05.294787 19 49 59.661 -25 08 26.95 19.8G 24OR F52 C~89YB 2023 08 05.300485 19 49 59.577 -25 08 26.88 19.7G 24OR F52 C~89YB 2023 08 05.306183 19 49 59.495 -25 08 26.78 19.8G 24OR F52 C~89YB 2023 08 18.276219 19 47 04.925 -25 03 50.96 20.0G 24OR F51 C~89YB 2023 08 18.281362 19 47 04.855 -25 03 50.85 20.0G 24OR F51 C~89YB 2023 08 18.286535 19 47 04.786 -25 03 50.68 19.9G 24OR F51 C~89YB 2023 08 18.291672 19 47 04.727 -25 03 50.68 19.8G 24OR F51 C~89YB 2023 09 11.263285 19 43 19.006 -24 49 33.22 20.1G 24OR F52 C~89YB 2023 09 11.268366 19 43 18.974 -24 49 32.96 20.2G 24OR F52 C~89YB 2023 09 11.273447 19 43 18.939 -24 49 32.74 20.2G 24OR F52 C~89YB 2023 09 11.278528 19 43 18.910 -24 49 32.50 20.1G 24OR F52 C~89YB 2024 06 02.569880 20 39 59.308 -18 27 34.55 19.9G 24OR F52 C~89YB 2024 06 02.580410 20 39 59.247 -18 27 34.23 19.9G 24OR F52 C~89YB 2024 06 02.590968 20 39 59.180 -18 27 33.99 20.1G 24OR F52 C~89YB 2024 06 02.601495 20 39 59.122 -18 27 33.70 20.0G 24OR F52 C~89YB 2024 06 07.509464 20 39 28.377 -18 25 34.02 19.9G 24OR F51 C~89YB 2024 06 07.521106 20 39 28.297 -18 25 33.76 19.8G 24OR F51 C~89YB 2024 06 07.532748 20 39 28.211 -18 25 33.49 19.8G 24OR F51 C~89YB 2024 06 07.544418 20 39 28.127 -18 25 33.25 19.7G 24OR F51 C~89YB 2024 06 11.534499 20 38 58.085 -18 24 12.66 19.9G 24OR F52 C~89YB 2024 06 11.545699 20 38 58.003 -18 24 12.62 19.7G 24OR F52 C~89YB 2024 06 11.556887 20 38 57.898 -18 24 12.23 19.8G 24OR F52 C~89YB 2024 06 11.568088 20 38 57.804 -18 24 12.01 19.8G 24OR F52 C~89YB 2024 06 15.555902 20 38 23.531 -18 23 05.49 20.0G 24OR F51 C~89YB 2024 06 15.566943 20 38 23.422 -18 23 05.29 20.0G 24OR F51 C~89YB 2024 06 15.577970 20 38 23.323 -18 23 05.16 19.9G 24OR F51 C~89YB 2024 06 15.588983 20 38 23.218 -18 23 05.02 19.8G 24OR F51 C~89YB 2024 06 29.506854 20 35 54.251 -18 20 47.41 19.6G 24OR F52 C~89YB 2024 07 05.486787 20 34 38.444 -18 20 25.96 19.6G 24OR F51 C~89YB 2024 07 05.497798 20 34 38.294 -18 20 26.02 19.4G 24OR F51 C~89YB 2024 07 05.508802 20 34 38.147 -18 20 26.04 19.5G 24OR F51 C~89YB 2024 07 05.519805 20 34 38.001 -18 20 25.88 19.5G 24OR F51 C~89YB 2024 07 27.387940 20 29 25.428 -18 20 54.19 19.9w 24OR F51 C~89YB 2024 07 27.399611 20 29 25.236 -18 20 54.21 19.9w 24OR F51 C~89YB 2024 07 27.411255 20 29 25.071 -18 20 54.17 19.6w 24OR F51 C~89YB 2024 07 27.85908 20 29 18.37 -18 20 55.8 19.7V 24OR M45 B~89YB 2024 07 27.86370 20 29 18.33 -18 20 55.5 19.6V 24OR M45 B~89YB 2024 07 27.86815 20 29 18.25 -18 20 55.6 19.5V 24OR M45 B~89YB 2024 07 28.529632 20 29 08.370 -18 20 57.46 19.3G 24OR T14 C~89YB 2024 07 28.530840 20 29 08.353 -18 20 57.46 19.4G 24OR T14 C~89YB 2024 07 28.532066 20 29 08.334 -18 20 57.44 19.4G 24OR T14 C~89YB 2024 07 28.542462 20 29 08.23 -18 20 56.8 19.4V 24OR Q20 B~89YB 2024 07 28.678756 20 29 06.13 -18 20 57.5 17.3V 24OR Q20 B~89YB 2024 07 28.909832 20 29 02.77 -18 20 58.8 19.3G 24OR I93 B~89YB 2024 07 28.95210 20 29 02.13 -18 20 59.0 24OR 204 B~8Al8 2024 07 28.97142 20 29 01.82 -18 20 58.8 20. G 24OR 204 B~8Al8 2024 07 28.977497 20 29 01.73 -18 20 58.7 19.2G 24OR I93 B~89YB 2024 07 29.119315 20 28 59.603 -18 20 58.70 19.6V 24OR Y05 B~89YB 2024 07 29.133366 20 28 59.384 -18 20 58.73 20.0V 24OR Y05 B~89YB 2024 07 29.146719 20 28 59.188 -18 20 58.99 19.8V 24OR Y05 B~89YB 2024 07 29.891698 20 28 48.10 -18 21 01.8 19.3G 24OR 595 C~89YB 2024 07 29.91815 20 28 47.64 -18 21 01.2 19.2G 24OR G02 C~89YB 2024 07 29.923841 20 28 47.61 -18 21 01.1 19.7G 24OR 595 C~89YB 2024 07 29.93528 20 28 47.42 -18 21 01.3 19.4G 24OR G02 C~89YB 2024 08 05.934166 20 27 03.953 -18 21 19.01 19.1o 24OR M22 C~8Al8 2024 08 05.937326 20 27 03.917 -18 21 18.76 19.1o 24OR M22 C~8Al8 2024 08 05.942779 20 27 03.934 -18 21 19.94 19.1o 24OR M22 C~8Al8 2024 08 05.952820 20 27 03.667 -18 21 19.80 19.3o 24OR M22 C~8Al8 2024 08 27.312088 20 22 16.769 -18 20 47.53 19.6w 24OR F51 C~8CRB 2024 08 27.322466 20 22 16.644 -18 20 47.46 19.6w 24OR F51 C~8CRB 2024 08 27.332865 20 22 16.516 -18 20 47.40 19.6w 24OR F51 C~8CRB 2024 08 27.343253 20 22 16.391 -18 20 47.35 19.5w 24OR F51 C~8CRB 2024 09 25.259193 20 18 18.807 -18 12 55.14 19.7w 24OR F51 C~8HfG 2024 09 25.271036 20 18 18.755 -18 12 54.80 19.8w 24OR F51 C~8HfG 2024 09 25.282837 20 18 18.705 -18 12 54.49 19.9w 24OR F51 C~8HfG 2024 09 25.294649 20 18 18.649 -18 12 54.11 20.0w 24OR F51 C~8HfG 2024 10 04.222810 20 17 54.633 -18 08 10.58 20.1w 24OR F51 C~8HfG 2024 10 04.234867 20 17 54.616 -18 08 10.19 20.0w 24OR F51 C~8HfG 2024 10 04.246685 20 17 54.595 -18 08 09.82 19.9w 24OR F51 C~8HfG 2024 10 04.258509 20 17 54.577 -18 08 09.32 19.8w 24OR F51 C~8HfG
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 0.07
2 3.3806 0.00 0.02 0.00 0.04
3 3.3809 0.00 0.02 0.00 0.07
4 3.3915 0.00 0.04 0.00 0.08
5 4.0740 0.00 -0.00 0.00 0.06
6 4.0740 0.00 0.05 0.00 0.01
7 4.3092 0.00 0.10 0.00 0.03
8 4.3092 0.00 -0.07 0.00 0.20
9 4.3092 0.00 0.07 0.00 0.09
10 4.3092 0.00 -0.29 0.00 0.05
11 6.2286 0.00 0.06 0.00 0.02
12 6.2286 0.00 -0.04 0.00 0.02
13 6.2482 0.00 0.10 0.00 -0.31
14 6.2482 0.00 0.24 0.00 -0.22
15 6.2482 0.00 0.24 0.00 -0.12
16 6.2482 0.00 0.08 0.00 -0.03
17 6.2482 0.00 -0.00 0.00 0.06
18 7.4927 0.00 -0.02 0.00 0.07
19 8.2381 0.00 -0.03 0.00 0.08
20 8.2381 0.00 -0.01 0.00 0.01
21 8.2411 0.00 -0.11 0.00 -0.01
22 8.4512 0.00 -0.12 0.00 -0.03
23 8.4512 0.00 -0.45 0.00 -0.19
24 10.3221 0.00 -0.03 0.00 -0.05
25 10.4468 0.00 0.14 0.00 0.01
26 10.4469 0.00 0.14 0.00 0.07
27 10.6386 0.00 -0.02 0.00 0.08
28 11.4061 0.00 -0.09 0.00 0.07
29 11.4118 0.00 -0.02 0.00 -0.06
30 11.4119 0.00 -0.02 0.00 -0.13
31 11.4119 0.00 0.00 0.00 -0.09
32 11.4119 0.00 -0.15 0.00 -0.10
33 11.4882 0.00 0.04 0.00 -0.02
34 11.4882 0.00 0.03 0.00 -0.05
35 11.4883 0.00 0.02 0.00 -0.03
36 11.4883 0.00 -0.00 0.00 -0.02
37 11.5288 0.00 0.07 0.00 -0.00
38 11.6107 0.00 -0.07 0.00 -0.03
39 12.2773 0.00 -0.21 0.00 0.02
40 12.2774 0.00 0.08 0.00 0.11
41 12.2774 0.00 0.07 0.00 0.04
42 12.3621 0.00 0.05 0.00 -0.04
43 12.3729 0.00 0.27 0.00 -0.18
44 12.3948 0.00 0.05 0.00 0.06
45 12.3949 0.00 0.00 0.00 -0.06
46 12.3949 0.00 0.03 0.00 0.01
47 12.3949 0.00 0.04 0.00 0.02
48 12.4984 0.00 0.02 0.00 0.01
49 12.4984 0.00 0.01 0.00 -0.01
50 12.4984 0.00 0.04 0.00 0.00
51 12.5339 0.00 0.09 0.00 0.04
52 12.5339 0.00 0.01 0.00 0.02
53 12.5339 0.00 -0.04 0.00 0.06
54 12.5339 0.00 0.04 0.00 -0.07
55 12.5996 0.00 0.03 0.00 -0.04
56 12.5996 0.00 0.04 0.00 -0.01
57 12.5996 0.00 0.01 0.00 -0.02
58 12.5996 0.00 0.06 0.00 -0.01
59 13.3259 0.00 0.02 0.00 -0.03
60 13.3260 0.00 0.03 0.00 0.01
61 13.3260 0.00 -0.05 0.00 -0.04
62 13.3260 0.00 0.01 0.00 -0.03
63 13.3395 0.00 -0.01 0.00 -0.03
64 13.3395 0.00 0.05 0.00 -0.02
65 13.3395 0.00 0.03 0.00 0.00
66 13.3396 0.00 0.05 0.00 -0.01
67 13.3505 0.00 0.01 0.00 -0.01
68 13.3505 0.00 0.19 0.00 -0.18
69 13.3506 0.00 0.02 0.00 0.01
70 13.3506 0.00 0.02 0.00 0.02
71 13.3615 0.00 0.04 0.00 -0.00
72 13.3615 0.00 -0.04 0.00 0.03
73 13.3616 0.00 0.03 0.00 -0.01
74 13.3616 0.00 0.02 0.00 -0.03
75 13.3997 0.00 -0.06 0.00 0.17
76 13.4161 0.00 0.04 0.00 0.02
77 13.4161 0.00 0.02 0.00 -0.07
78 13.4161 0.00 0.04 0.00 -0.11
79 13.4162 0.00 0.08 0.00 0.03
80 13.4760 0.00 0.17 0.00 -0.08
81 13.4761 0.00 -0.05 0.00 -0.06
82 13.4761 0.00 0.13 0.00 0.02
83 13.4773 0.00 -0.45 0.00 -0.09
84 13.4773 0.00 0.00 0.00 0.22
85 13.4773 0.00 -0.19 0.00 0.14
86 13.4792 0.00 0.07 0.00 -0.00
87 13.4792 0.00 0.09 0.00 -0.00
88 13.4792 0.00 0.08 0.00 0.02
89 13.4792 0.00 0.11 0.00 0.03
90 13.4796 0.00 -0.38 0.00 -0.27
91 13.4802 0.00 0.28 0.00 0.00
92 13.4803 0.00 0.35 0.00 -0.04
93 13.4804 0.00 0.08 0.00 0.22
94 13.4804 0.00 0.02 0.00 0.33
95 13.4808 0.00 -0.12 0.00 0.04
96 13.4808 0.00 -0.20 0.00 0.05
97 13.4808 0.00 -0.10 0.00 -0.17
98 13.4829 0.00 -0.36 0.00 -0.09
99 13.4830 0.00 -1.21 0.00 0.61
100 13.4830 0.00 -0.43 0.00 0.71
101 13.4830 0.00 -0.63 0.00 0.57
102 13.5022 0.00 -0.19 0.00 0.02
103 13.5022 0.00 -0.02 0.00 0.28
104 13.5022 0.00 1.45 0.00 -0.89
105 13.5022 0.00 -0.31 0.00 -0.73
106 13.5607 0.00 0.07 0.00 -0.01
107 13.5607 0.00 0.07 0.00 -0.00
108 13.5608 0.00 0.04 0.00 -0.01
109 13.5608 0.00 0.05 0.00 -0.02
110 13.6400 0.00 0.04 0.00 -0.01
111 13.6400 0.00 0.05 0.00 -0.00
112 13.6400 0.00 0.08 0.00 -0.02
113 13.6400 0.00 0.02 0.00 0.03
114 13.6645 0.00 0.08 0.00 0.05
115 13.6645 0.00 0.10 0.00 0.01
116 13.6646 0.00 0.06 0.00 -0.05
117 13.6646 0.00 0.06 0.00 0.03
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.