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: 620086 # Created Sun Nov 24 02:07:44 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 74 observations of 74 # Arc: 12.07y # First observation: 2011/01/25 # Last observation: 2023/02/20 # Chi-squared of fit: 56.92 DOF: 142 RMS: 0.16 # Min/Max residuals: -0.40 0.54 # Exact a, adot, b, bdot, g, gdot: 1.520141E-05 2.510905E-02 8.638452E-06 1.292488E-02 2.535620E-02 7.801388E-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 -4.339356 113.794350 -0.191860 -0.073276 -0.965720 2455586.822776 # Heliocentric elements and errors Epoch: 2455586.5000 = 2011/01/25 Mean Anomaly: 20.14193 +/- 0.000 Argument of Peri: 297.26722 +/- 0.000 Long of Asc Node: 122.21035 +/- 0.000 Inclination: 27.58825 +/- 0.000 Eccentricity: 0.44611733 +/- 0.0000 Semi-Major Axis: 63.80796608 +/- 0.0000 Time of Perihelion: 2445170.3006 +/- 0.0 Perihelion: 35.34212674 +/- 0.0000 Aphelion: 92.27380543 +/- 0.0000 Period (y) 509.7069 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -16.42858698 +/- 0.0000 Ecliptic Y 36.79036937 +/- 0.0000 Ecliptic Z -2.98371013 +/- 0.0000 Ecliptic XDOT -0.00286323 +/- 0.0000 Ecliptic YDOT -0.00022256 +/- 0.0000 Ecliptic ZDOT 0.00132785 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 40.40193603 +/- 0.0000 Geocenter to KBO 39.43793122 +/- 0.0000 # Hcoef: 6.67
The following table shows the complete astrometric record for 620086. 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 (620086) followed by the observatory code and reference code for the source of the astrometry.
2011 01 25.32201 07 39 32.921 +17 04 03.94 23.3G 620086 F51 C~36pk 2011 01 25.33486 07 39 32.847 +17 04 04.56 23.5G 620086 F51 C~36pk 2011 01 25.34773 07 39 32.774 +17 04 04.96 22.5G 620086 F51 C~36pk 2012 05 08.27127 07 43 23.865 +17 58 48.41 22.7G 620086 F51 C~36pk 2013 02 10.40882 07 50 59.201 +18 06 14.38 22.6G 620086 F51 C~36pk 2013 02 10.42420 07 50 59.149 +18 06 14.65 22.3G 620086 F51 C~36pk 2013 02 10.43966 07 50 59.059 +18 06 14.92 23.4G 620086 F51 C~36pk 2013 02 10.45509 07 50 58.996 +18 06 15.28 22.3G 620086 F51 C~36pk 2013 12 31.54023 08 00 41.149 +18 17 46.73 22.4w 620086 F51 C~2VWB 2013 12 31.55612 08 00 41.067 +18 17 47.40 22.1w 620086 F51 C~2VWB 2013 12 31.58531 08 00 40.923 +18 17 47.92 22.7w 620086 F51 C~2VWB 2014 10 28.58436 08 09 33.895 +18 28 51.47 23.3G 620086 F51 C~36pk 2014 12 21.58605 08 07 39.250 +18 39 16.74 22.5G 620086 F51 C~36pk 2014 12 21.59991 08 07 39.201 +18 39 17.27 22.6G 620086 F51 C~36pk 2014 12 21.65060 08 07 38.978 +18 39 18.23 22.9G 620086 F51 C~36pk 2014 12 21.65257 08 07 38.971 +18 39 18.54 22.4G 620086 F51 C~36pk 2014 12 21.65454 08 07 38.962 +18 39 18.37 23.1G 620086 F51 C~36pk 2014 12 21.65719 08 07 38.936 +18 39 18.34 22.8G 620086 F51 C~36pk 2015 01 14.37076 08 05 46.548 +18 47 29.77 22.4G 620086 F51 C~36pk 2015 01 14.38311 08 05 46.482 +18 47 29.94 22.6G 620086 F51 C~36pk 2015 01 14.39535 08 05 46.419 +18 47 30.27 23.0G 620086 F51 C~36pk 2015 01 14.40757 08 05 46.372 +18 47 30.63 22.2G 620086 F51 C~36pk 2015 01 16.52663 08 05 35.607 +18 48 17.38 22.6w 620086 F51 C~1vYC 2015 01 16.53888 08 05 35.545 +18 48 17.86 23.0w 620086 F51 C~1vYC 2015 01 16.55114 08 05 35.487 +18 48 18.04 22.7w 620086 F51 C~1vYC 2015 01 16.56344 08 05 35.433 +18 48 18.24 22.7w 620086 F51 C~1vYC 2015 02 16.27974 08 03 05.952 +18 59 34.22 22.2G 620086 F51 C~36pk 2015 02 16.29205 08 03 05.901 +18 59 34.20 22.1G 620086 F51 C~36pk 2015 02 17.29180 08 03 01.569 +18 59 55.18 22.5w 620086 F51 C~1vYC 2015 02 17.30420 08 03 01.527 +18 59 55.53 22.5w 620086 F51 C~1vYC 2015 02 17.31657 08 03 01.449 +18 59 55.47 22.4w 620086 F51 C~1vYC 2015 03 16.36558 08 01 29.641 +19 08 12.08 22.9G 620086 F51 C~36pk 2015 03 16.37792 08 01 29.578 +19 08 12.11 22.9G 620086 F51 C~36pk 2015 03 16.39020 08 01 29.582 +19 08 12.19 22.7G 620086 F51 C~36pk 2015 03 16.40241 08 01 29.573 +19 08 12.83 22.9G 620086 F51 C~36pk 2015 03 17.34182 08 01 27.386 +19 08 27.02 22.7w 620086 F51 C~1vYC 2015 03 17.35424 08 01 27.365 +19 08 27.34 22.8w 620086 F51 C~1vYC 2015 03 17.36674 08 01 27.314 +19 08 27.52 22.8w 620086 F51 C~1vYC 2015 04 10.29593 08 01 00.674 +19 13 14.78 22.9w 620086 F51 C~1vYC 2015 04 10.31953 08 01 00.661 +19 13 14.96 22.6w 620086 F51 C~1vYC 2015 04 10.33127 08 01 00.684 +19 13 15.15 22.7w 620086 F51 C~1vYC 2016 01 03.40904 08 12 49.883 +19 07 11.36 23.1G 620086 F51 C~36pk 2016 01 03.42069 08 12 49.822 +19 07 11.71 23.4G 620086 F51 C~36pk 2016 01 03.43231 08 12 49.776 +19 07 11.84 23.6G 620086 F51 C~36pk 2016 01 03.44396 08 12 49.727 +19 07 11.98 22.8G 620086 F51 C~36pk 2016 01 07.38714 08 12 30.853 +19 08 38.08 22.7G 620086 F51 C~36pk 2016 01 07.39960 08 12 30.750 +19 08 38.21 22.4G 620086 F51 C~36pk 2016 01 07.41203 08 12 30.710 +19 08 38.42 22.5G 620086 F51 C~36pk 2016 01 07.42452 08 12 30.633 +19 08 38.61 22.6G 620086 F51 C~36pk 2016 02 11.27862 08 09 38.460 +19 21 40.98 22.8G 620086 F51 C~36pk 2016 02 11.29029 08 09 38.384 +19 21 41.02 22.6G 620086 F51 C~36pk 2016 02 11.30220 08 09 38.342 +19 21 41.44 22.6G 620086 F51 C~36pk 2016 02 11.31383 08 09 38.298 +19 21 41.51 22.8G 620086 F51 C~36pk 2016 03 03.23492 08 08 12.766 +19 28 41.00 23.2G 620086 F51 C~36pk 2016 03 03.24659 08 08 12.718 +19 28 41.18 22.8G 620086 F51 C~36pk 2016 03 03.26009 08 08 12.669 +19 28 41.41 23.1G 620086 F51 C~36pk 2016 03 03.27174 08 08 12.612 +19 28 41.95 23.2G 620086 F51 C~36pk 2016 11 08.58542 08 21 29.011 +19 15 02.91 23.6G 620086 F51 C~36pk 2017 01 05.43638 08 18 39.977 +19 30 48.23 22.5G 620086 F51 C~36pk 2017 01 28.48453 08 16 46.013 +19 39 37.97 23.1G 620086 F51 C~36pk 2017 01 28.49745 08 16 45.953 +19 39 38.31 22.9G 620086 F51 C~36pk 2017 01 28.51039 08 16 45.867 +19 39 38.62 23.0G 620086 F51 C~36pk 2017 01 28.52333 08 16 45.828 +19 39 39.03 23.2G 620086 F51 C~36pk 2017 11 20.54544 08 27 10.059 +19 38 03.88 22.6G 620086 F51 C~36pk 2017 12 12.51750 08 26 16.791 +19 43 49.32 21.7G 620086 F51 C~36pk 2017 12 20.47581 08 25 48.147 +19 46 25.39 22.9R 620086 G37 C~2VWB 2017 12 20.51622 08 25 47.967 +19 46 26.26 620086 G37 C~2VWB 2018 01 16.34786 08 23 47.244 +19 56 27.82 22.8G 620086 F51 C~36pk 2018 01 16.35949 08 23 47.194 +19 56 27.94 22.8G 620086 F51 C~36pk 2018 01 16.37112 08 23 47.128 +19 56 28.30 22.7G 620086 F51 C~36pk 2018 01 16.38280 08 23 47.073 +19 56 28.46 23.0G 620086 F51 C~36pk 2023 02 20.145540 08 49 51.080 +21 42 42.17 22.9G 620086 G37 C~6Ent 2023 02 20.190320 08 49 50.878 +21 42 42.80 620086 G37 C~6Ent 2023 02 20.236050 08 49 50.682 +21 42 44.07 620086 G37 C~6Ent
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 0.08 0.00 -0.13
2 0.0000 0.00 -0.04 0.00 0.21
3 0.0001 0.00 -0.13 0.00 0.34
4 1.2839 0.00 -0.11 0.00 0.03
5 2.0454 0.00 -0.08 0.00 0.10
6 2.0455 0.00 0.21 0.00 0.04
7 2.0455 0.00 -0.07 0.00 -0.01
8 2.0455 0.00 0.06 0.00 0.02
9 2.9328 0.00 -0.00 0.00 -0.38
10 2.9329 0.00 -0.07 0.00 -0.03
11 2.9330 0.00 -0.09 0.00 -0.09
12 3.7570 0.00 0.23 0.00 -0.36
13 3.9049 0.00 -0.11 0.00 -0.37
14 3.9049 0.00 0.06 0.00 -0.09
15 3.9051 0.00 0.00 0.00 -0.08
16 3.9051 0.00 0.02 0.00 0.20
17 3.9051 0.00 0.02 0.00 -0.01
18 3.9051 0.00 -0.20 0.00 -0.09
19 3.9700 0.00 0.01 0.00 -0.01
20 3.9701 0.00 -0.03 0.00 -0.12
21 3.9701 0.00 -0.03 0.00 -0.06
22 3.9701 0.00 0.20 0.00 0.03
23 3.9759 0.00 -0.05 0.00 -0.09
24 3.9760 0.00 -0.04 0.00 0.12
25 3.9760 0.00 0.04 0.00 0.03
26 3.9760 0.00 0.18 0.00 -0.04
27 4.0601 0.00 -0.20 0.00 0.19
28 4.0602 0.00 -0.14 0.00 -0.09
29 4.0629 0.00 -0.17 0.00 0.07
30 4.0629 0.00 0.01 0.00 0.16
31 4.0630 0.00 -0.34 0.00 -0.16
32 4.1370 0.00 0.23 0.00 -0.01
33 4.1370 0.00 -0.27 0.00 -0.17
34 4.1371 0.00 0.24 0.00 -0.27
35 4.1371 0.00 0.54 0.00 0.18
36 4.1397 0.00 -0.06 0.00 -0.05
37 4.1397 0.00 0.06 0.00 0.08
38 4.1398 0.00 -0.27 0.00 0.08
39 4.2053 0.00 0.04 0.00 0.02
40 4.2053 0.00 -0.15 0.00 0.00
41 4.2054 0.00 0.20 0.00 0.09
42 4.9393 0.00 -0.03 0.00 -0.00
43 4.9394 0.00 -0.11 0.00 0.09
44 4.9394 0.00 0.04 0.00 -0.03
45 4.9394 0.00 0.14 0.00 -0.14
46 4.9502 0.00 0.39 0.00 0.21
47 4.9502 0.00 -0.23 0.00 0.06
48 4.9503 0.00 0.09 0.00 -0.01
49 4.9503 0.00 -0.14 0.00 -0.09
50 5.0457 0.00 0.12 0.00 0.12
51 5.0458 0.00 -0.20 0.00 -0.10
52 5.0458 0.00 0.01 0.00 0.06
53 5.0458 0.00 0.17 0.00 -0.12
54 5.1031 0.00 0.19 0.00 0.02
55 5.1031 0.00 0.09 0.00 -0.02
56 5.1032 0.00 0.06 0.00 -0.03
57 5.1032 0.00 -0.18 0.00 0.29
58 5.7885 0.00 -0.40 0.00 0.08
59 5.9469 0.00 0.17 0.00 -0.24
60 6.0100 0.00 -0.11 0.00 -0.06
61 6.0101 0.00 -0.03 0.00 -0.01
62 6.0101 0.00 -0.34 0.00 0.00
63 6.0101 0.00 0.06 0.00 0.12
64 6.8206 0.00 0.33 0.00 0.02
65 6.8808 0.00 0.02 0.00 0.26
66 6.9025 0.00 0.15 0.00 0.10
67 6.9027 0.00 -0.17 0.00 0.15
68 6.9761 0.00 -0.10 0.00 0.14
69 6.9761 0.00 0.02 0.00 -0.02
70 6.9762 0.00 -0.10 0.00 0.06
71 6.9762 0.00 -0.05 0.00 -0.05
72 12.0707 0.00 -0.02 0.00 0.10
73 12.0708 0.00 -0.04 0.00 -0.23
74 12.0709 0.00 0.10 0.00 0.06
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.
620086 quality flag:3 Type: SCATNEAR SCATNEAR SCATNEAR axisobj 64.377 64.377 64.377 ecceobj 0.451 0.451 0.451 incobj 27.562 27.562 27.562 qmin 34.508 34.528 34.471 qmax 93.984 94.368 94.247 amean 63.533 63.747 63.616 amin 62.701 62.929 62.673 amax 64.630 64.761 64.741 emean 0.436 0.439 0.438 emin 0.417 0.421 0.416 emax 0.456 0.458 0.457 imean 26.433 26.407 26.410 imin 25.652 25.699 25.687 imax 27.254 27.273 27.300 excite_mean 0.623 0.625 0.624 fracstop 1.000 1.000 1.000 cjmean 2.816 2.815 2.815 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 201.7 198.5 196.6 kozaiamp 180.0 180.0 180.0