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: 612733 # Created Sun Nov 24 02:07:42 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 39 observations of 39 # Arc: 18.19y # First observation: 2003/12/24 # Last observation: 2022/03/02 # Chi-squared of fit: 49.25 DOF: 72 RMS: 0.20 # Min/Max residuals: -0.44 0.64 # Exact a, adot, b, bdot, g, gdot: 1.854015E-05 2.763144E-02 7.113537E-07 2.274213E-03 2.587066E-02 1.473349E-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 -1.285087 111.999228 0.335753 -0.020595 -0.921142 2452997.968413 # Heliocentric elements and errors Epoch: 2452998.5000 = 2003/12/25 Mean Anomaly: 12.51982 +/- 0.000 Argument of Peri: 327.34408 +/- 0.000 Long of Asc Node: 126.48839 +/- 0.000 Inclination: 4.84711 +/- 0.000 Eccentricity: 0.16510333 +/- 0.0000 Semi-Major Axis: 47.09180925 +/- 0.0000 Time of Perihelion: 2448893.5088 +/- 0.0 Perihelion: 39.31679454 +/- 0.0000 Aphelion: 54.86682397 +/- 0.0000 Period (y) 323.1664 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -14.51374682 +/- 0.0000 Ecliptic Y 36.81306703 +/- 0.0000 Ecliptic Z -0.86687570 +/- 0.0000 Ecliptic XDOT -0.00277594 +/- 0.0000 Ecliptic YDOT -0.00095217 +/- 0.0000 Ecliptic ZDOT 0.00023727 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 39.58029794 +/- 0.0000 Geocenter to KBO 38.65383600 +/- 0.0000 # Hcoef: 6.90
The following table shows the complete astrometric record for 612733. 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 (612733) followed by the observatory code and reference code for the source of the astrometry.
2003 12 24.46767 07 34 11.14 +20 22 26.1 23.0g 612733 568 Cq9908 2003 12 24.49091 07 34 11.03 +20 22 26.4 23.0g 612733 568 Cq9908 2003 12 24.51415 07 34 10.91 +20 22 26.7 22.8g 612733 568 Cq9908 2003 12 25.50897 07 34 05.84 +20 22 38.8 23.0g 612733 568 Cq9908 2004 04 15.15900 07 28 06.38 +20 40 05.3 612733 675 Cq9908 2004 04 15.21134 07 28 06.46 +20 40 05.2 612733 675 Cq9908 2004 04 16.19869 07 28 08.04 +20 40 05.0 612733 675 Cq9908 2004 09 16.51192 07 42 18.47 +20 11 38.1 612733 675 Cq9908 2004 09 18.46447 07 42 26.14 +20 11 18.1 612733 675 Cq9908 2004 09 18.47321 07 42 26.20 +20 11 17.9 612733 675 Cq9908 2005 01 08.36606 07 39 34.48 +20 18 03.4 612733 568 Cq9908 2005 01 08.40392 07 39 34.27 +20 18 04.0 612733 568 Cq9908 2005 01 08.44177 07 39 34.07 +20 18 04.7 612733 568 Cq9908 2005 01 15.38895 07 38 56.35 +20 19 43.4 23.1r 612733 568 Cq9908 2005 10 03.45349 07 49 43.76 +20 00 25.5 23.6R 612733 675 Cq9908 2005 10 03.52662 07 49 43.97 +20 00 25.0 612733 675 Cq9908 2008 09 27.39060 08 08 41.85 +19 29 50.7 24.7R 612733 250 S~06Ah 2008 09 27.39754 08 08 41.88 +19 29 50.7 612733 250 S~06Ah 2008 09 27.40379 08 08 41.90 +19 29 50.6 612733 250 S~06Ah 2008 09 27.41074 08 08 41.92 +19 29 50.5 612733 250 S~06Ah 2013 03 13.17100 08 27 21.04 +19 03 27.4 22.5R 612733 695 C~0ud7 2013 03 14.15788 08 27 17.96 +19 03 39.7 612733 695 C~0ud7 2013 03 14.24696 08 27 17.69 +19 03 40.4 612733 695 C~0ud7 2014 01 28.41175 08 37 03.82 +18 35 39.4 22.3R 612733 G37 C~16Mq 2014 01 28.48111 08 37 03.46 +18 35 40.7 612733 G37 C~16Mq 2018 12 09.478230 09 11 45.75 +16 52 50.7 22.0r 612733 568 C~2rbK 2018 12 09.542090 09 11 45.61 +16 52 51.5 22.0r 612733 568 C~2rbK 2018 12 09.583950 09 11 45.51 +16 52 51.9 22.1r 612733 568 C~2rbK 2020 01 04.356170 09 16 28.26 +16 40 26.9 22.9G 612733 705 C~3slk 2020 01 04.398230 09 16 28.08 +16 40 27.7 23.3G 612733 705 C~3slk 2020 01 04.469940 09 16 27.79 +16 40 29.4 22.9G 612733 705 C~3slk 2021 02 15.247490 09 19 09.987 +16 37 05.21 22.9G 612733 G37 C~4Yr4 2021 02 15.300110 09 19 09.743 +16 37 06.44 612733 G37 C~4Yr4 2021 03 20.142160 09 16 48.427 +16 48 10.94 23.0G 612733 G37 C~4hj3 2021 03 20.183330 09 16 48.285 +16 48 11.84 612733 G37 C~4hj3 2021 03 20.222410 09 16 48.160 +16 48 12.52 612733 G37 C~4hj3 2022 03 02.145700 09 24 01.590 +16 22 31.83 23.0G 612733 G37 C~5Rkz 2022 03 02.185550 09 24 01.451 +16 22 32.96 612733 G37 C~5Rkz 2022 03 02.226300 09 24 01.260 +16 22 33.67 612733 G37 C~5Rkz
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 -0.34 0.00 0.19
2 0.0001 0.00 -0.18 0.00 0.21
3 0.0001 0.00 -0.18 0.00 0.23
4 0.0029 0.00 -0.29 0.00 0.27
5 0.3085 0.00 -0.01 0.00 -0.27
6 0.3087 0.00 0.03 0.00 -0.35
7 0.3114 0.00 0.03 0.00 -0.32
8 0.7311 0.00 0.38 0.00 0.64
9 0.7365 0.00 -0.44 0.00 0.24
10 0.7365 0.00 -0.04 0.00 0.12
11 1.0428 0.00 0.17 0.00 -0.35
12 1.0429 0.00 0.14 0.00 -0.29
13 1.0431 0.00 0.27 0.00 -0.12
14 1.0621 0.00 0.14 0.00 0.02
15 1.7768 0.00 -0.00 0.00 0.07
16 1.7770 0.00 0.37 0.00 0.07
17 4.7609 0.00 0.04 0.00 -0.15
18 4.7609 0.00 0.12 0.00 -0.07
19 4.7609 0.00 0.09 0.00 -0.11
20 4.7610 0.00 0.02 0.00 -0.13
21 9.2175 0.00 -0.16 0.00 -0.08
22 9.2202 0.00 -0.28 0.00 0.14
23 9.2205 0.00 -0.12 0.00 -0.23
24 10.0970 0.00 0.04 0.00 0.11
25 10.0972 0.00 0.10 0.00 0.00
26 14.9596 0.00 -0.12 0.00 -0.05
27 14.9598 0.00 -0.07 0.00 -0.02
28 14.9599 0.00 -0.14 0.00 -0.12
29 16.0298 0.00 0.04 0.00 -0.17
30 16.0299 0.00 -0.08 0.00 -0.22
31 16.0301 0.00 -0.04 0.00 0.04
32 17.1466 0.00 -0.08 0.00 0.07
33 17.1467 0.00 0.19 0.00 0.06
34 17.2366 0.00 0.04 0.00 -0.14
35 17.2367 0.00 0.06 0.00 0.12
36 17.2368 0.00 0.22 0.00 0.18
37 18.1867 0.00 -0.36 0.00 -0.02
38 18.1868 0.00 0.28 0.00 0.24
39 18.1869 0.00 0.21 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.
612733 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 46.972 46.972 46.972 ecceobj 0.164 0.164 0.164 incobj 4.857 4.857 4.857 qmin 38.296 38.284 38.290 qmax 55.763 55.698 55.791 amean 46.799 46.799 46.799 amin 46.399 46.402 46.401 amax 47.288 47.261 47.277 emean 0.165 0.165 0.165 emin 0.151 0.151 0.151 emax 0.180 0.179 0.180 imean 3.650 3.650 3.650 imin 3.102 3.102 3.102 imax 4.228 4.225 4.227 excite_mean 0.177 0.177 0.177 fracstop 1.000 1.000 1.000 cjmean 3.097 3.097 3.097 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 173.1 173.1 173.1 kozaiamp 180.0 179.9 179.9