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: 612236 # Created Sun Apr 28 01:09:11 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 116 observations of 116 # Arc: 20.05y # First observation: 2000/08/26 # Last observation: 2020/09/13 # Chi-squared of fit: 157.28 DOF: 226 RMS: 0.21 # Min/Max residuals: -1.15 0.94 # Exact a, adot, b, bdot, g, gdot: 1.534642E-05 2.225447E-02 6.635436E-09 -4.046495E-04 2.351536E-02 -6.342013E-04 # 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 -0.459308 -13.097633 0.243597 -0.007999 -0.977595 2451782.719823 # Heliocentric elements and errors Epoch: 2451782.5000 = 2000/08/26 Mean Anomaly: 258.63256 +/- 0.000 Argument of Peri: 308.94508 +/- 0.000 Long of Asc Node: 143.25704 +/- 0.000 Inclination: 1.13340 +/- 0.000 Eccentricity: 0.03814636 +/- 0.0000 Semi-Major Axis: 43.12433563 +/- 0.0000 Time of Perihelion: 2480908.3124 +/- 0.0 Perihelion: 41.47929934 +/- 0.0000 Aphelion: 44.76937192 +/- 0.0000 Period (y) 283.1991 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 42.32054523 +/- 0.0000 Ecliptic Y -10.09025778 +/- 0.0000 Ecliptic Z -0.34091293 +/- 0.0000 Ecliptic XDOT 0.00050759 +/- 0.0000 Ecliptic YDOT 0.00254578 +/- 0.0000 Ecliptic ZDOT -0.00004637 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 43.50816159 +/- 0.0000 Geocenter to KBO 42.52545564 +/- 0.0000 # Hcoef: 6.58
The following table shows the complete astrometric record for 612236. 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 (612236) followed by the observatory code and reference code for the source of the astrometry.
2000 08 26.21908 23 12 31.14 -05 35 41.3 22.3R 612236 807 Cg3217 2000 08 26.27600 23 12 30.90 -05 35 42.9 612236 807 Cg3217 2001 05 23.33702 23 19 30.45 -04 51 37.7 22.3R 612236 807 Ch1433 2001 05 23.34067 23 19 30.46 -04 51 37.8 22.1R 612236 807 Ch1433 2001 08 19.23948 23 17 46.00 -05 03 54.9 21.3R 612236 807 Cd7925 2001 08 19.32335 23 17 45.65 -05 03 57.1 612236 807 Cd7925 2001 08 20.29469 23 17 41.82 -05 04 22.0 21.2R 612236 807 Cd7925 2001 08 20.38078 23 17 41.38 -05 04 24.4 612236 807 Cd7925 2002 08 11.37222 23 23 01.19 -04 31 52.9 21.3R 612236 807 Cg3217 2002 08 12.31262 23 22 57.81 -04 32 15.2 612236 807 Cg3217 2002 08 12.39073 23 22 57.52 -04 32 17.1 612236 807 Cg3217 2002 09 11.36111 23 20 55.19 -04 45 29.0 22.0R 612236 662 Cg3217 2002 09 11.44646 23 20 54.84 -04 45 32.0 612236 662 Cg3217 2007 11 11.13277 23 40 58.20 -02 43 46.9 22.5R 612236 688 Cw6710 2007 11 11.20714 23 40 58.10 -02 43 48.1 612236 688 Cw6710 2008 10 30.246674 23 46 12.36 -02 11 23.1 612236 645 C~1GLG 2008 10 30.247504 23 46 12.36 -02 11 23.1 612236 645 C~1GLG 2008 10 30.249991 23 46 12.35 -02 11 23.2 612236 645 C~1GLG 2012 08 25.49965 00 09 44.870 +00 16 18.07 23.3G 612236 F51 C~2r78 2012 10 05.46588 00 06 54.242 -00 02 26.62 22.9G 612236 F51 C~2r78 2012 10 22.32425 00 05 46.071 -00 09 46.64 22.4G 612236 F51 C~2r78 2013 09 08.188183 00 13 40.78 +00 40 23.6 23.5g 612236 W84 C~351I 2013 09 08.18871 00 13 40.788 +00 40 23.56 23.8g 612236 W84 C~4yCS 2013 09 11.308125 00 13 27.86 +00 38 58.2 23.6g 612236 W84 C~351I 2013 09 11.30866 00 13 27.865 +00 38 58.10 24.4g 612236 W84 C~4yCS 2013 09 29.46884 00 12 09.657 +00 30 24.14 22.7G 612236 F51 C~2r78 2013 09 30.16242 00 12 06.66 +00 30 05.3 22.3r 612236 W84 C~3cV0 2013 10 04.151088 00 11 49.37 +00 28 12.7 23.7g 612236 W84 C~351I 2013 10 04.15162 00 11 49.380 +00 28 12.60 23.8g 612236 W84 C~4yCS 2013 10 13.09613 00 11 11.502 +00 24 07.21 22.2z 612236 W84 C~4yCS 2013 10 13.09613 00 11 11.50 +00 24 07.2 22.5z 612236 W84 C~3cV0 2013 10 13.11063 00 11 11.45 +00 24 06.8 22.6i 612236 W84 C~3cV0 2013 10 22.40930 00 10 34.352 +00 20 07.86 23.5G 612236 F51 C~2r78 2013 10 28.071597 00 10 13.39 +00 17 54.4 22.8r 612236 W84 C~351I 2013 10 28.07212 00 10 13.408 +00 17 54.44 22.8r 612236 W84 C~4yCS 2013 11 22.06844 00 09 02.79 +00 10 31.5 24.1g 612236 W84 C~3cV0 2013 11 22.06844 00 09 02.792 +00 10 31.55 23.9g 612236 W84 C~4yCS 2013 11 22.07119 00 09 02.77 +00 10 31.3 22.3i 612236 W84 C~3cV0 2013 11 22.07119 00 09 02.772 +00 10 31.31 22.2i 612236 W84 C~4yCS 2014 01 20.23909 00 09 35.538 +00 14 57.48 22.4G 612236 F51 C~2r78 2014 07 27.59105 00 20 38.906 +01 24 57.05 22.9G 612236 F51 C~2r78 2014 07 29.54486 00 20 35.507 +01 24 32.32 23.2G 612236 F51 C~2r78 2014 07 30.60477 00 20 33.549 +01 24 18.75 22.9G 612236 F51 C~2r78 2014 08 18.30786 00 19 46.26 +01 18 52.3 22.7i 612236 W84 C~3cV0 2014 08 27.53783 00 19 15.113 +01 15 22.47 22.8G 612236 F51 C~2r78 2014 09 18.43141 00 17 47.427 +01 05 41.04 22.7G 612236 F51 C~2r78 2014 09 20.48152 00 17 38.592 +01 04 43.25 22.6G 612236 F51 C~2r78 2014 09 20.49310 00 17 38.530 +01 04 42.99 22.6G 612236 F51 C~2r78 2014 09 20.50459 00 17 38.494 +01 04 42.50 23.3G 612236 F51 C~2r78 2014 09 20.51609 00 17 38.426 +01 04 42.24 22.5G 612236 F51 C~2r78 2014 10 29.14146 00 14 57.96 +00 47 24.5 22.3z 612236 W84 C~3cV0 2014 10 29.14146 00 14 57.961 +00 47 24.45 22.2z 612236 W84 C~4yCS 2014 11 12.33713 00 14 12.392 +00 42 36.83 23.6G 612236 F51 C~2r78 2014 11 15.10154 00 14 04.97 +00 41 50.8 22.8z 612236 W84 C~3cV0 2014 11 15.10154 00 14 04.970 +00 41 50.79 22.8z 612236 W84 C~4yCS 2015 06 26.59016 00 25 33.786 +01 56 11.20 24.1G 612236 F51 C~2r78 2015 07 30.55303 00 25 20.130 +01 53 57.35 22.9G 612236 F51 C~2r78 2015 07 31.49861 00 25 18.436 +01 53 45.11 22.4G 612236 F51 C~2r78 2015 11 01.28799 00 19 35.394 +01 16 07.41 22.6G 612236 F51 C~2r78 2015 11 01.30096 00 19 35.341 +01 16 07.14 23.1G 612236 F51 C~2r78 2015 11 01.31291 00 19 35.301 +01 16 06.92 22.8G 612236 F51 C~2r78 2015 11 01.32487 00 19 35.270 +01 16 06.65 23.5G 612236 F51 C~2r78 2015 11 02.34898 00 19 31.695 +01 15 43.98 22.5G 612236 F51 C~2r78 2015 12 09.29848 00 18 08.696 +01 07 15.67 23.0G 612236 F51 C~2r78 2016 08 14.58203 00 29 31.161 +02 19 23.89 22.8G 612236 F51 C~2r78 2016 09 09.32882 00 28 01.63 +02 09 25.5 22.5i 612236 W84 C~3cV0 2016 09 09.32882 00 28 01.635 +02 09 25.52 22.4i 612236 W84 C~4yCS 2016 09 09.33021 00 28 01.62 +02 09 25.4 23.2r 612236 W84 C~3cV0 2016 09 09.331065 00 28 01.62 +02 09 25.4 23.7g 612236 W84 C~351I 2016 09 09.33159 00 28 01.623 +02 09 25.22 23.9g 612236 W84 C~4yCS 2016 09 11.17158 00 27 54.141 +02 08 35.99 22.1z 612236 W84 C~4yCS 2016 09 11.17158 00 27 54.14 +02 08 36.0 22.3z 612236 W84 C~3cV0 2016 09 30.45993 00 26 31.453 +01 59 35.39 22.5G 612236 F51 C~2r78 2016 10 02.18024 00 26 23.91 +01 58 46.8 22.0i 612236 W84 C~3cV0 2016 10 02.18163 00 26 23.90 +01 58 46.8 22.3r 612236 W84 C~3cV0 2016 10 02.18301 00 26 23.894 +01 58 46.84 23.2g 612236 W84 C~4yCS 2016 10 02.18301 00 26 23.89 +01 58 46.8 23.5g 612236 W84 C~3cV0 2016 10 09.38647 00 25 52.540 +01 55 23.96 22.8G 612236 F51 C~2r78 2016 11 30.10104 00 23 04.02 +01 37 44.1 23.2r 612236 W84 C~3cV0 2016 11 30.10240 00 23 04.01 +01 37 44.0 22.7i 612236 W84 C~3cV0 2016 11 30.10240 00 23 04.015 +01 37 44.01 22.5i 612236 W84 C~4yCS 2016 12 05.09034 00 22 56.92 +01 37 03.0 22.3z 612236 W84 C~3cV0 2016 12 05.09034 00 22 56.923 +01 37 03.01 22.2z 612236 W84 C~4yCS 2016 12 05.09170 00 22 56.926 +01 37 02.94 22.1Y 612236 W84 C~4yCS 2017 07 30.54206 00 34 52.555 +02 52 54.65 23.1G 612236 F51 C~2r78 2017 07 30.55199 00 34 52.538 +02 52 54.47 23.2G 612236 F51 C~2r78 2017 07 30.56192 00 34 52.526 +02 52 54.71 23.3G 612236 F51 C~2r78 2017 07 30.57191 00 34 52.484 +02 52 54.12 22.9G 612236 F51 C~2r78 2017 08 24.54438 00 33 50.318 +02 45 47.11 23.2G 612236 F51 C~2r78 2017 08 27.33896 00 33 40.937 +02 44 44.32 22.2G 612236 F51 C~2r78 2017 09 15.45939 00 32 27.372 +02 36 38.23 22.9G 612236 F51 C~2r78 2017 09 15.47153 00 32 27.322 +02 36 38.01 22.6G 612236 F51 C~2r78 2017 09 15.48369 00 32 27.269 +02 36 37.73 22.7G 612236 F51 C~2r78 2017 09 22.43226 00 31 57.669 +02 33 24.03 23.0G 612236 F51 C~2r78 2017 10 22.183808 00 29 49.59 +02 19 40.1 23.3r 612236 W84 C~351I 2017 10 22.18433 00 29 49.592 +02 19 40.13 23.3r 612236 W84 C~4yCS 2017 10 22.185185 00 29 49.58 +02 19 40.2 22.7i 612236 W84 C~351I 2017 10 22.18571 00 29 49.581 +02 19 40.19 22.5i 612236 W84 C~4yCS 2017 10 22.186562 00 29 49.57 +02 19 40.2 23.8g 612236 W84 C~351I 2017 10 22.18709 00 29 49.574 +02 19 40.17 23.9g 612236 W84 C~4yCS 2017 10 27.175139 00 29 29.82 +02 17 34.7 22.1z 612236 W84 C~351I 2017 10 27.17567 00 29 29.816 +02 17 34.67 22.1z 612236 W84 C~4yCS 2017 10 29.132928 00 29 22.34 +02 16 47.4 22.0z 612236 W84 C~351I 2017 10 29.13345 00 29 22.326 +02 16 47.26 22.1z 612236 W84 C~4yCS 2018 09 09.32306 00 37 44.088 +03 09 20.25 22.5i 612236 W84 C~4yCS 2018 09 09.32583 00 37 44.074 +03 09 20.30 23.1g 612236 W84 C~4yCS 2018 11 26.06971 00 32 46.647 +02 37 47.67 23.4g 612236 W84 C~4yCS 2019 11 01.24217 00 38 53.46 +03 15 27.0 23.4g 612236 T09 C~7dBw 2019 11 01.24260 00 38 53.46 +03 15 27.0 23.4g 612236 T09 C~71v6 2019 11 01.30637 00 38 53.24 +03 15 25.2 23.8g 612236 T09 C~7dBw 2019 11 01.30680 00 38 53.24 +03 15 25.2 23.8g 612236 T09 C~71v6 2019 11 01.50333 00 38 52.44 +03 15 20.8 24.0g 612236 T09 C~7dBw 2019 11 01.50376 00 38 52.44 +03 15 20.8 24.0g 612236 T09 C~71v6 2020 09 13.46449 00 47 10.116 +04 06 59.32 22.5w 612236 F51 C~47sn 2020 09 13.47648 00 47 10.056 +04 06 58.71 22.5w 612236 F51 C~47sn 2020 09 13.48852 00 47 10.001 +04 06 58.41 22.5w 612236 F51 C~47sn
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 -0.05 0.00 -0.08
2 0.0002 0.00 -0.02 0.00 -0.16
3 0.7395 0.00 0.28 0.00 0.36
4 0.7396 0.00 0.31 0.00 0.21
5 0.9802 0.00 0.15 0.00 0.22
6 0.9804 0.00 -0.04 0.00 0.17
7 0.9831 0.00 0.23 0.00 0.20
8 0.9833 0.00 -1.15 0.00 0.02
9 1.9580 0.00 0.36 0.00 -0.12
10 1.9606 0.00 0.20 0.00 -0.28
11 1.9608 0.00 0.16 0.00 -0.34
12 2.0428 0.00 -0.81 0.00 0.94
13 2.0431 0.00 -0.43 0.00 0.31
14 7.2085 0.00 -0.34 0.00 0.17
15 7.2087 0.00 0.72 0.00 -0.00
16 8.1780 0.00 0.30 0.00 -0.42
17 8.1780 0.00 0.34 0.00 -0.41
18 8.1780 0.00 0.30 0.00 -0.46
19 11.9980 0.00 0.06 0.00 -0.11
20 12.1102 0.00 0.08 0.00 -0.31
21 12.1563 0.00 0.33 0.00 -0.16
22 13.0348 0.00 -0.18 0.00 0.03
23 13.0348 0.00 -0.03 0.00 0.01
24 13.0434 0.00 -0.14 0.00 0.07
25 13.0434 0.00 -0.03 0.00 -0.02
26 13.0931 0.00 -0.22 0.00 -0.54
27 13.0950 0.00 0.01 0.00 0.12
28 13.1059 0.00 -0.12 0.00 -0.01
29 13.1059 0.00 0.06 0.00 -0.10
30 13.1304 0.00 -0.02 0.00 -0.14
31 13.1304 0.00 0.01 0.00 -0.13
32 13.1304 0.00 0.15 0.00 -0.16
33 13.1559 0.00 -0.02 0.00 -0.36
34 13.1714 0.00 -0.40 0.00 -0.14
35 13.1714 0.00 -0.10 0.00 -0.09
36 13.2398 0.00 0.19 0.00 0.10
37 13.2398 0.00 0.16 0.00 0.05
38 13.2398 0.00 -0.03 0.00 -0.11
39 13.2398 0.00 -0.06 0.00 -0.12
40 13.4018 0.00 0.06 0.00 -0.09
41 13.9175 0.00 0.15 0.00 0.15
42 13.9229 0.00 -0.11 0.00 -0.31
43 13.9258 0.00 -0.06 0.00 0.05
44 13.9770 0.00 0.13 0.00 -0.10
45 14.0022 0.00 0.02 0.00 0.03
46 14.0622 0.00 0.11 0.00 -0.17
47 14.0678 0.00 0.12 0.00 0.00
48 14.0678 0.00 -0.05 0.00 0.07
49 14.0679 0.00 0.17 0.00 -0.09
50 14.0679 0.00 -0.09 0.00 -0.02
51 14.1736 0.00 0.19 0.00 -0.05
52 14.1736 0.00 0.17 0.00 0.00
53 14.2125 0.00 -0.17 0.00 -0.10
54 14.2201 0.00 -0.02 0.00 -0.04
55 14.2201 0.00 -0.02 0.00 -0.03
56 14.8320 0.00 -0.87 0.00 0.26
57 14.9249 0.00 -0.07 0.00 0.10
58 14.9275 0.00 -0.03 0.00 -0.00
59 15.1816 0.00 0.02 0.00 0.00
60 15.1816 0.00 -0.08 0.00 0.02
61 15.1816 0.00 -0.03 0.00 0.07
62 15.1817 0.00 0.15 0.00 0.07
63 15.1845 0.00 0.27 0.00 0.06
64 15.2856 0.00 -0.08 0.00 -0.02
65 15.9681 0.00 0.13 0.00 0.01
66 16.0386 0.00 0.09 0.00 0.12
67 16.0386 0.00 0.01 0.00 0.10
68 16.0386 0.00 -0.05 0.00 0.04
69 16.0386 0.00 0.00 0.00 0.06
70 16.0386 0.00 0.08 0.00 -0.10
71 16.0437 0.00 -0.02 0.00 0.03
72 16.0437 0.00 -0.01 0.00 0.02
73 16.0965 0.00 0.26 0.00 -0.08
74 16.1012 0.00 0.17 0.00 0.02
75 16.1012 0.00 0.11 0.00 0.06
76 16.1012 0.00 0.05 0.00 0.09
77 16.1012 0.00 0.11 0.00 0.13
78 16.1209 0.00 0.20 0.00 0.03
79 16.2625 0.00 0.02 0.00 0.05
80 16.2625 0.00 -0.02 0.00 -0.03
81 16.2625 0.00 -0.09 0.00 -0.04
82 16.2762 0.00 -0.10 0.00 -0.00
83 16.2762 0.00 -0.15 0.00 -0.01
84 16.2762 0.00 -0.03 0.00 -0.06
85 16.9263 0.00 0.08 0.00 -0.01
86 16.9263 0.00 0.07 0.00 -0.07
87 16.9263 0.00 0.14 0.00 0.28
88 16.9264 0.00 -0.23 0.00 -0.19
89 16.9947 0.00 0.08 0.00 0.04
90 17.0024 0.00 0.02 0.00 0.10
91 17.0547 0.00 0.02 0.00 -0.02
92 17.0548 0.00 0.05 0.00 0.09
93 17.0548 0.00 0.03 0.00 0.14
94 17.0738 0.00 -0.10 0.00 -0.38
95 17.1553 0.00 -0.03 0.00 -0.03
96 17.1553 0.00 0.03 0.00 0.01
97 17.1553 0.00 -0.10 0.00 0.10
98 17.1553 0.00 -0.05 0.00 0.11
99 17.1553 0.00 -0.16 0.00 0.14
100 17.1553 0.00 -0.07 0.00 0.12
101 17.1689 0.00 0.05 0.00 0.07
102 17.1689 0.00 0.02 0.00 0.05
103 17.1743 0.00 0.14 0.00 0.14
104 17.1743 0.00 -0.04 0.00 0.01
105 18.0372 0.00 -0.01 0.00 0.07
106 18.0373 0.00 -0.06 0.00 0.19
107 18.2501 0.00 -0.07 0.00 0.12
108 19.1814 0.00 -0.11 0.00 0.16
109 19.1814 0.00 -0.08 0.00 0.17
110 19.1816 0.00 0.32 0.00 -0.12
111 19.1816 0.00 0.35 0.00 -0.11
112 19.1822 0.00 -0.26 0.00 0.16
113 19.1822 0.00 -0.24 0.00 0.17
114 20.0500 0.00 0.07 0.00 0.28
115 20.0500 0.00 -0.09 0.00 -0.01
116 20.0500 0.00 -0.17 0.00 0.00
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.
612236 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 43.204 43.204 43.204 ecceobj 0.037 0.037 0.037 incobj 1.133 1.133 1.133 qmin 39.910 39.917 39.907 qmax 46.272 46.266 46.268 amean 42.995 42.995 42.995 amin 42.663 42.663 42.659 amax 43.355 43.345 43.343 emean 0.047 0.047 0.047 emin 0.026 0.026 0.027 emax 0.068 0.068 0.068 imean 1.917 1.917 1.917 imin 0.699 0.699 0.699 imax 2.712 2.712 2.712 excite_mean 0.058 0.058 0.058 fracstop 1.000 1.000 1.000 cjmean 3.085 3.085 3.085 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 189.5 189.6 189.5 kozaiamp 180.0 180.0 180.0