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: 673087 # Created Fri Nov 22 02:07:50 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 114 observations of 114 # Arc: 13.97y # First observation: 2010/02/25 # Last observation: 2024/02/15 # Chi-squared of fit: 88.32 DOF: 222 RMS: 0.16 # Min/Max residuals: -0.58 0.73 # Exact a, adot, b, bdot, g, gdot: 1.543103E-05 2.184775E-02 -2.278266E-07 -9.588610E-04 2.332404E-02 -2.767471E-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 -27.300427 160.556400 0.070758 -0.454994 -0.881507 2455252.894476 # Heliocentric elements and errors Epoch: 2455252.5000 = 2010/02/25 Mean Anomaly: 270.75375 +/- 0.000 Argument of Peri: 8.93018 +/- 0.000 Long of Asc Node: 255.99257 +/- 0.000 Inclination: 26.81506 +/- 0.000 Eccentricity: 0.12881139 +/- 0.0000 Semi-Major Axis: 43.11796985 +/- 0.0000 Time of Perihelion: 2480889.8625 +/- 0.0 Perihelion: 37.56388406 +/- 0.0000 Aphelion: 48.67205564 +/- 0.0000 Period (y) 283.1364 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -36.83404227 +/- 0.0000 Ecliptic Y 13.07592709 +/- 0.0000 Ecliptic Z -19.66453894 +/- 0.0000 Ecliptic XDOT -0.00053035 +/- 0.0000 Ecliptic YDOT -0.00252579 +/- 0.0000 Ecliptic ZDOT 0.00004892 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 43.75417428 +/- 0.0000 Geocenter to KBO 42.87433584 +/- 0.0000 # Hcoef: 4.80
The following table shows the complete astrometric record for 673087. 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 (673087) followed by the observatory code and reference code for the source of the astrometry.
2010 02 25.39371 10 06 14.295 -17 38 47.98 21.2G 673087 F51 C~2kRK 2010 12 16.63045 10 15 16.626 -18 06 22.00 21.4G 673087 F51 C~2kRK 2011 03 25.06266 10 09 00.491 -17 56 36.13 21.5R 673087 809 C~0UX7 2011 03 25.14645 10 09 00.168 -17 56 32.85 21.1R 673087 809 C~0UX7 2011 03 25.22775 10 08 59.832 -17 56 30.12 21.0R 673087 809 C~0UX7 2011 03 26.01131 10 08 56.928 -17 55 59.44 20.9R 673087 809 C~0UX7 2011 03 26.12723 10 08 56.484 -17 55 55.16 21.3R 673087 809 C~0UX7 2011 03 26.23556 10 08 56.063 -17 55 51.27 21.2R 673087 809 C~0UX7 2011 05 26.01557 10 07 26.43 -17 15 57.3 673087 807 C~0evL 2011 05 26.04498 10 07 26.47 -17 15 56.6 673087 807 C~0evL 2011 12 05.63688 10 20 09.969 -18 30 42.82 21.4G 673087 F51 C~2kRK 2012 01 28.52358 10 17 58.768 -18 49 19.97 20.9G 673087 F51 C~2kRK 2012 01 28.53570 10 17 58.713 -18 49 20.02 20.8G 673087 F51 C~2kRK 2012 02 02.46132 10 17 37.480 -18 49 04.22 21.5G 673087 F51 C~2kRK 2012 02 04.46351 10 17 28.602 -18 48 51.92 21.9G 673087 F51 C~2kRK 2012 02 04.47611 10 17 28.545 -18 48 51.77 22.0G 673087 F51 C~2kRK 2012 12 22.65477 10 24 41.794 -19 11 51.30 21.8G 673087 F51 C~2kRK 2013 03 20.36358 10 18 56.639 -19 03 28.02 20.7i 673087 F51 C~2FaT 2013 03 20.37616 10 18 56.590 -19 03 27.64 20.9i 673087 F51 C~2FaT 2013 03 20.38928 10 18 56.542 -19 03 27.16 20.9r 673087 F51 C~2FaT 2013 03 20.40078 10 18 56.490 -19 03 26.64 20.8r 673087 F51 C~2FaT 2013 05 05.29408 10 16 53.006 -18 31 56.26 21.6G 673087 F51 C~2kRK 2013 12 15.62374 10 29 44.316 -19 38 35.20 21.9G 673087 F51 C~2kRK 2015 01 06.54686 10 34 02.340 -20 19 09.33 21.0i 673087 F51 C~1vY1 2015 01 06.55984 10 34 02.318 -20 19 09.48 20.6i 673087 F51 C~1vY1 2015 01 06.57284 10 34 02.281 -20 19 09.79 20.6i 673087 F51 C~1vY1 2015 02 02.49318 10 32 26.057 -20 23 03.42 21.0i 673087 F51 C~1vY1 2015 02 02.50451 10 32 25.996 -20 23 03.20 21.1i 673087 F51 C~1vY1 2015 02 02.52707 10 32 25.912 -20 23 03.11 21.3i 673087 F51 C~1vY1 2015 03 25.37508 10 28 33.240 -20 03 57.74 21.2i 673087 F51 C~1vY1 2015 03 25.38686 10 28 33.195 -20 03 57.36 21.1i 673087 F51 C~1vY1 2015 03 25.39862 10 28 33.150 -20 03 57.20 21.5i 673087 F51 C~1vY1 2015 03 25.41038 10 28 33.092 -20 03 56.62 21.1i 673087 F51 C~1vY1 2015 04 23.25144 10 27 00.458 -19 43 51.32 20.9G 673087 F51 C~2kRK 2015 04 26.24133 10 26 54.293 -19 41 41.49 21.7G 673087 F51 C~2kRK 2015 04 26.24230 10 26 54.296 -19 41 41.29 21.6G 673087 F51 C~2kRK 2015 06 11.25875 10 26 58.403 -19 13 22.18 21.7G 673087 F51 C~2kRK 2016 02 12.49811 10 36 46.836 -20 52 47.10 20.9G 673087 F51 C~2kRK 2016 02 12.50887 10 36 46.782 -20 52 46.96 21.0G 673087 F51 C~2kRK 2016 02 12.51961 10 36 46.739 -20 52 46.85 20.9G 673087 F51 C~2kRK 2016 02 12.53041 10 36 46.684 -20 52 46.76 21.0G 673087 F51 C~2kRK 2016 03 02.43331 10 35 17.078 -20 47 04.64 20.5G 673087 F51 C~2kRK 2016 03 02.44543 10 35 17.035 -20 47 04.18 20.8G 673087 F51 C~2kRK 2016 03 02.45754 10 35 16.965 -20 47 03.95 20.8G 673087 F51 C~2kRK 2016 03 12.39212 10 34 30.269 -20 42 20.18 21.3G 673087 F51 C~2kRK 2016 03 12.40377 10 34 30.219 -20 42 19.78 21.2G 673087 F51 C~2kRK 2016 03 12.41544 10 34 30.162 -20 42 19.49 21.0G 673087 F51 C~2kRK 2016 03 12.42708 10 34 30.108 -20 42 19.06 21.0G 673087 F51 C~2kRK 2016 04 12.32463 10 32 28.240 -20 22 28.14 20.6G 673087 F51 C~2kRK 2016 04 12.33496 10 32 28.204 -20 22 27.56 20.7G 673087 F51 C~2kRK 2016 04 12.34530 10 32 28.167 -20 22 27.15 20.8G 673087 F51 C~2kRK 2016 04 12.35566 10 32 28.140 -20 22 26.76 20.9G 673087 F51 C~2kRK 2017 03 16.34812 10 39 20.979 -21 11 13.38 21.7G 673087 F51 C~2kRK 2017 04 25.25238 10 36 59.330 -20 44 08.95 20.9G 673087 F51 C~2kRK 2017 04 25.26333 10 36 59.302 -20 44 08.47 21.0G 673087 F51 C~2kRK 2017 04 25.27430 10 36 59.272 -20 44 07.99 21.1G 673087 F51 C~2kRK 2017 04 28.26308 10 36 53.046 -20 41 56.33 21.2G 673087 F51 C~2kRK 2017 04 28.27467 10 36 53.028 -20 41 55.80 21.3G 673087 F51 C~2kRK 2017 12 26.57512 10 49 40.177 -21 44 14.15 21.5G 673087 F51 C~2kRK 2017 12 26.58611 10 49 40.155 -21 44 14.39 21.5G 673087 F51 C~2kRK 2017 12 26.59710 10 49 40.135 -21 44 14.65 21.2G 673087 F51 C~2kRK 2017 12 26.60811 10 49 40.116 -21 44 15.03 21.2G 673087 F51 C~2kRK 2018 01 09.56537 10 49 11.545 -21 50 16.17 21.1G 673087 F51 C~2kRK 2018 01 09.57571 10 49 11.514 -21 50 16.31 21.4G 673087 F51 C~2kRK 2018 01 09.58604 10 49 11.496 -21 50 16.60 21.4G 673087 F51 C~2kRK 2018 01 09.59636 10 49 11.460 -21 50 16.79 21.5G 673087 F51 C~2kRK 2019 12 11.61994 11 00 13.206 -22 31 56.99 21.0i 673087 F51 C~3VYC 2019 12 11.63119 11 00 13.202 -22 31 57.42 21.4i 673087 F51 C~3VYC 2019 12 11.64231 11 00 13.209 -22 31 57.91 21.3i 673087 F51 C~3VYC 2019 12 12.60130 11 00 13.471 -22 32 38.31 20.8i 673087 F51 C~3VYC 2019 12 12.61219 11 00 13.475 -22 32 38.80 20.3i 673087 F51 C~3VYC 2019 12 12.62318 11 00 13.462 -22 32 39.39 21.2i 673087 F51 C~3VYC 2019 12 30.61087 11 00 01.701 -22 43 35.36 21.4w 673087 F51 C~3Z9I 2019 12 30.62179 11 00 01.684 -22 43 35.73 21.4w 673087 F51 C~3Z9I 2019 12 30.63267 11 00 01.670 -22 43 36.04 21.5w 673087 F51 C~3Z9I 2019 12 30.64358 11 00 01.653 -22 43 36.35 21.4w 673087 F51 C~3Z9I 2020 01 20.52442 10 59 11.382 -22 51 17.99 21.1w 673087 F51 C~3cq6 2020 01 20.53469 10 59 11.349 -22 51 18.06 21.0w 673087 F51 C~3cq6 2020 01 20.54500 10 59 11.314 -22 51 18.15 21.0w 673087 F51 C~3cq6 2020 01 20.55525 10 59 11.275 -22 51 18.31 20.9w 673087 F51 C~3cq6 2020 04 28.27478 10 52 25.046 -22 12 06.40 21.2w 673087 F51 C~3qNF 2020 04 28.28505 10 52 25.018 -22 12 05.93 21.2w 673087 F51 C~3qNF 2020 04 28.29531 10 52 24.995 -22 12 05.47 21.3w 673087 F51 C~3qNF 2020 04 28.30557 10 52 24.969 -22 12 05.05 21.3w 673087 F51 C~3qNF 2021 01 17.54953 11 04 39.262 -23 19 03.46 20.8w 673087 F51 C~4UFs 2021 01 17.56051 11 04 39.229 -23 19 03.64 20.9w 673087 F51 C~4UFs 2021 01 17.57153 11 04 39.187 -23 19 03.77 20.8w 673087 F51 C~4UFs 2021 01 17.58253 11 04 39.162 -23 19 04.02 20.8w 673087 F51 C~4UFs 2021 02 07.54535 11 03 21.921 -23 21 30.38 21.0w 673087 F51 C~4ZFn 2021 02 07.55566 11 03 21.862 -23 21 30.42 21.1w 673087 F51 C~4ZFn 2021 02 07.56596 11 03 21.829 -23 21 30.49 21.3w 673087 F51 C~4ZFn 2021 02 07.57632 11 03 21.779 -23 21 30.39 21.2w 673087 F51 C~4ZFn 2022 03 11.399840 11 06 19.371 -23 41 39.17 21.0w 673087 F52 C~5Vg2 2022 03 11.410758 11 06 19.322 -23 41 38.88 21.0w 673087 F52 C~5Vg2 2022 03 11.421696 11 06 19.262 -23 41 38.85 21.0w 673087 F52 C~5Vg2 2022 04 09.297304 11 04 09.249 -23 24 22.37 20.9w 673087 F52 C~5Xi8 2022 04 09.308160 11 04 09.192 -23 24 21.84 21.0w 673087 F52 C~5Xi9 2022 04 09.319064 11 04 09.165 -23 24 21.34 21.0w 673087 F52 C~5Xi9 2022 04 09.329900 11 04 09.110 -23 24 20.88 21.0w 673087 F52 C~5Xi9 2023 03 27.392763 11 10 34.872 -24 01 08.44 20.7w 673087 F52 C~6bzi 2023 03 27.403576 11 10 34.824 -24 01 08.12 20.7w 673087 F52 C~6bzi 2023 03 27.414380 11 10 34.770 -24 01 07.65 20.8w 673087 F52 C~6bzi 2023 03 28.361064 11 10 30.450 -24 00 32.76 20.8w 673087 F51 C~6bzi 2023 03 28.372644 11 10 30.400 -24 00 32.27 20.8w 673087 F51 C~6bzi 2023 03 28.384227 11 10 30.350 -24 00 31.86 20.7w 673087 F51 C~6bzi 2023 03 28.395804 11 10 30.295 -24 00 31.60 20.8w 673087 F51 C~6bzi 2024 02 14.509120 11 19 26.714 -24 43 30.24 20.9w 673087 F52 C~7myA 2024 02 14.520170 11 19 26.662 -24 43 30.35 21.0w 673087 F52 C~7myA 2024 02 14.531222 11 19 26.619 -24 43 30.31 20.9w 673087 F52 C~7myA 2024 02 14.542257 11 19 26.578 -24 43 30.22 20.9w 673087 F52 C~7myA 2024 02 15.453058 11 19 22.541 -24 43 25.17 20.8w 673087 F51 C~7myA 2024 02 15.464690 11 19 22.485 -24 43 25.13 20.9w 673087 F51 C~7myA 2024 02 15.476337 11 19 22.431 -24 43 24.99 20.8w 673087 F51 C~7myA 2024 02 15.487997 11 19 22.380 -24 43 25.11 20.9w 673087 F51 C~7myA
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 -0.16 0.00 -0.03
2 0.8056 0.00 -0.10 0.00 -0.06
3 1.0751 0.00 0.49 0.00 0.29
4 1.0753 0.00 0.52 0.00 0.37
5 1.0755 0.00 0.19 0.00 -0.02
6 1.0777 0.00 0.73 0.00 0.59
7 1.0780 0.00 0.72 0.00 0.42
8 1.0783 0.00 0.60 0.00 0.11
9 1.2447 0.00 -0.37 0.00 0.33
10 1.2448 0.00 -0.24 0.00 0.09
11 1.7748 0.00 -0.16 0.00 -0.01
12 1.9223 0.00 -0.22 0.00 0.12
13 1.9224 0.00 -0.26 0.00 0.06
14 1.9358 0.00 -0.22 0.00 -0.05
15 1.9413 0.00 -0.20 0.00 -0.06
16 1.9414 0.00 -0.19 0.00 0.00
17 2.8234 0.00 -0.08 0.00 -0.14
18 3.0636 0.00 -0.18 0.00 0.06
19 3.0636 0.00 -0.11 0.00 -0.02
20 3.0636 0.00 0.00 0.00 -0.02
21 3.0637 0.00 -0.05 0.00 0.08
22 3.1893 0.00 -0.17 0.00 -0.58
23 3.8035 0.00 0.11 0.00 -0.03
24 4.8628 0.00 -0.27 0.00 -0.15
25 4.8629 0.00 -0.06 0.00 -0.04
26 4.8629 0.00 -0.08 0.00 -0.09
27 4.9366 0.00 0.09 0.00 -0.38
28 4.9366 0.00 -0.07 0.00 -0.19
29 4.9367 0.00 0.15 0.00 -0.17
30 5.0759 0.00 -0.18 0.00 0.05
31 5.0760 0.00 -0.12 0.00 -0.02
32 5.0760 0.00 -0.06 0.00 -0.31
33 5.0760 0.00 -0.19 0.00 -0.17
34 5.1550 0.00 -0.04 0.00 -0.06
35 5.1632 0.00 -0.10 0.00 -0.02
36 5.1632 0.00 -0.02 0.00 0.13
37 5.2892 0.00 -0.08 0.00 0.22
38 5.9633 0.00 0.02 0.00 -0.03
39 5.9634 0.00 -0.03 0.00 -0.01
40 5.9634 0.00 0.08 0.00 -0.01
41 5.9634 0.00 0.01 0.00 -0.03
42 6.0152 0.00 -0.20 0.00 -0.28
43 6.0152 0.00 0.04 0.00 -0.13
44 6.0152 0.00 -0.13 0.00 -0.20
45 6.0424 0.00 -0.03 0.00 0.01
46 6.0425 0.00 0.04 0.00 0.04
47 6.0425 0.00 0.01 0.00 -0.04
48 6.0425 0.00 0.02 0.00 0.02
49 6.1271 0.00 0.00 0.00 -0.18
50 6.1271 0.00 -0.05 0.00 -0.05
51 6.1272 0.00 -0.12 0.00 -0.08
52 6.1272 0.00 -0.03 0.00 -0.14
53 7.0526 0.00 0.06 0.00 -0.04
54 7.1618 0.00 -0.01 0.00 0.01
55 7.1619 0.00 -0.05 0.00 0.00
56 7.1619 0.00 -0.12 0.00 0.00
57 7.1701 0.00 -0.03 0.00 -0.04
58 7.1701 0.00 0.06 0.00 -0.02
59 7.8335 0.00 0.04 0.00 -0.11
60 7.8335 0.00 -0.04 0.00 -0.01
61 7.8335 0.00 -0.09 0.00 0.08
62 7.8336 0.00 -0.13 0.00 0.04
63 7.8718 0.00 -0.07 0.00 -0.04
64 7.8718 0.00 -0.11 0.00 0.03
65 7.8718 0.00 0.04 0.00 -0.05
66 7.8719 0.00 -0.08 0.00 -0.03
67 9.7912 0.00 0.09 0.00 -0.09
68 9.7912 0.00 -0.01 0.00 -0.04
69 9.7912 0.00 0.06 0.00 -0.06
70 9.7939 0.00 0.16 0.00 0.00
71 9.7939 0.00 0.19 0.00 -0.03
72 9.7939 0.00 -0.02 0.00 -0.16
73 9.8432 0.00 0.03 0.00 -0.05
74 9.8432 0.00 0.04 0.00 -0.09
75 9.8432 0.00 0.09 0.00 -0.07
76 9.8433 0.00 0.09 0.00 -0.05
77 9.9004 0.00 0.04 0.00 -0.05
78 9.9005 0.00 0.06 0.00 0.02
79 9.9005 0.00 0.05 0.00 0.06
80 9.9005 0.00 -0.02 0.00 0.04
81 10.1708 0.00 0.00 0.00 0.10
82 10.1708 0.00 -0.05 0.00 0.11
83 10.1708 0.00 -0.03 0.00 0.10
84 10.1709 0.00 -0.05 0.00 0.06
85 10.8943 0.00 0.04 0.00 0.03
86 10.8944 0.00 0.05 0.00 0.03
87 10.8944 0.00 -0.07 0.00 0.08
88 10.8944 0.00 0.06 0.00 0.01
89 10.9518 0.00 0.16 0.00 0.11
90 10.9518 0.00 -0.04 0.00 0.05
91 10.9519 0.00 0.14 0.00 -0.05
92 10.9519 0.00 0.07 0.00 0.03
93 12.0383 0.00 0.09 0.00 0.08
94 12.0384 0.00 0.16 0.00 0.07
95 12.0384 0.00 0.08 0.00 -0.20
96 12.1175 0.00 0.08 0.00 -0.02
97 12.1175 0.00 -0.13 0.00 0.05
98 12.1175 0.00 0.12 0.00 0.09
99 12.1176 0.00 -0.06 0.00 0.09
100 13.0814 0.00 0.01 0.00 0.07
101 13.0815 0.00 0.05 0.00 -0.01
102 13.0815 0.00 -0.01 0.00 0.07
103 13.0841 0.00 -0.03 0.00 0.06
104 13.0841 0.00 0.03 0.00 0.12
105 13.0842 0.00 0.08 0.00 0.10
106 13.0842 0.00 0.06 0.00 -0.07
107 13.9688 0.00 -0.11 0.00 0.19
108 13.9689 0.00 -0.15 0.00 0.02
109 13.9689 0.00 -0.05 0.00 0.00
110 13.9689 0.00 0.09 0.00 0.04
111 13.9714 0.00 0.03 0.00 0.07
112 13.9714 0.00 -0.02 0.00 0.04
113 13.9715 0.00 -0.04 0.00 0.12
114 13.9715 0.00 -0.01 0.00 -0.07
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.
673087 quality flag:3 Type: SCATEXTD SCATEXTD SCATEXTD axisobj 43.167 43.167 43.167 ecceobj 0.126 0.126 0.126 incobj 26.794 26.794 26.794 qmin 36.923 36.923 36.923 qmax 50.041 50.039 50.042 amean 43.345 43.345 43.345 amin 42.993 43.000 42.989 amax 43.720 43.726 43.720 emean 0.132 0.132 0.132 emin 0.119 0.118 0.119 emax 0.145 0.145 0.145 imean 28.221 28.225 28.222 imin 27.899 27.899 27.899 imax 28.541 28.563 28.542 excite_mean 0.491 0.491 0.491 fracstop 1.000 1.000 1.000 cjmean 2.790 2.790 2.790 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 165.0 164.9 164.8 kozaiamp 180.0 180.0 179.9