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: 612582 # Created Sun Nov 24 02:07:42 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 37 observations of 37 # Arc: 15.15y # First observation: 2003/08/25 # Last observation: 2018/10/18 # Chi-squared of fit: 28.66 DOF: 68 RMS: 0.16 # Min/Max residuals: -0.60 0.40 # Exact a, adot, b, bdot, g, gdot: 1.465259E-05 2.385746E-02 -8.305341E-07 -2.019687E-04 2.429206E-02 7.973394E-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 -2.968394 -3.582584 0.427292 -0.047627 -0.919599 2452876.779843 # Heliocentric elements and errors Epoch: 2452876.5000 = 2003/08/25 Mean Anomaly: 39.87810 +/- 0.000 Argument of Peri: 217.50602 +/- 0.000 Long of Asc Node: 95.97882 +/- 0.000 Inclination: 2.94959 +/- 0.000 Eccentricity: 0.03283033 +/- 0.0000 Semi-Major Axis: 43.15173325 +/- 0.0000 Time of Perihelion: 2441407.4417 +/- 0.0 Perihelion: 41.73504755 +/- 0.0000 Aphelion: 44.56841895 +/- 0.0000 Period (y) 283.4690 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 41.91968996 +/- 0.0000 Ecliptic Y -3.04865157 +/- 0.0000 Ecliptic Z -2.13182214 +/- 0.0000 Ecliptic XDOT 0.00025116 +/- 0.0000 Ecliptic YDOT 0.00267236 +/- 0.0000 Ecliptic ZDOT -0.00002721 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 42.08441744 +/- 0.0000 Geocenter to KBO 41.16572761 +/- 0.0000 # Hcoef: 7.01
The following table shows the complete astrometric record for 612582. 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 (612582) followed by the observatory code and reference code for the source of the astrometry.
2003 08 25.27910 23 51 34.52 -04 08 53.1 22.2R 612582 807 Ci4592 2003 08 25.38190 23 51 34.12 -04 08 56.1 612582 807 Ci4592 2003 09 03.13413 23 50 58.52 -04 13 02.3 23.0R 612582 304 Ci4592 2003 09 03.20601 23 50 58.25 -04 13 04.0 612582 304 Ci4592 2003 10 22.15921 23 47 30.57 -04 35 00.5 22.5R 612582 695 Cj4700 2003 10 22.25323 23 47 30.23 -04 35 02.5 612582 695 Cj4700 2004 08 13.30947 23 57 16.35 -03 32 05.9 21.5R 612582 807 Cl8405 2004 08 13.38192 23 57 16.10 -03 32 07.5 612582 807 Cl8405 2004 10 11.21987 23 53 12.16 -03 59 13.1 23.0R 612582 695 Cl8405 2004 10 11.31032 23 53 11.82 -03 59 15.6 612582 695 Cl8405 2010 09 16.42927 00 25 07.34 -00 34 16.9 23.5R 612582 688 C~0NG0 2010 09 16.47315 00 25 07.12 -00 34 18.0 612582 688 C~0NG0 2013 10 05.32455 00 38 40.97 +00 53 16.1 22.8R 612582 695 C~0zdV 2013 10 05.36866 00 38 40.77 +00 53 15.1 612582 695 C~0zdV 2013 10 06.36532 00 38 36.35 +00 52 47.4 612582 695 C~0zdV 2013 10 13.15009 00 38 06.427 +00 49 40.60 22.7i 612582 W84 C~4yD2 2013 11 23.12179 00 35 38.374 +00 35 37.72 23.4r 612582 W84 C~4yD2 2013 11 23.12459 00 35 38.361 +00 35 37.84 23.1i 612582 W84 C~4yD2 2014 11 13.07078 00 41 03.491 +01 09 57.86 24.0r 612582 W84 C~4yD2 2014 11 14.13129 00 41 00.075 +01 09 39.75 23.0i 612582 W84 C~4yD2 2016 09 01.37155 00 55 51.011 +02 44 12.46 23.1i 612582 W84 C~4yD2 2016 09 01.37293 00 55 51.011 +02 44 12.15 23.1r 612582 W84 C~4yD2 2016 11 05.19246 00 51 20.938 +02 15 50.25 23.4r 612582 W84 C~4yD2 2016 11 05.19523 00 51 20.933 +02 15 49.98 24.8g 612582 W84 C~4yD2 2016 11 06.15830 00 51 17.323 +02 15 29.85 22.4z 612582 W84 C~4yD2 2017 08 28.28539 01 01 00.570 +03 17 21.87 22.8i 612582 W84 C~4yD2 2017 08 28.28676 01 01 00.569 +03 17 22.02 23.4r 612582 W84 C~4yD2 2017 09 18.29705 00 59 43.521 +03 08 35.11 23.9r 612582 W84 C~4yD2 2017 09 24.28844 00 59 18.296 +03 05 50.54 23.0i 612582 W84 C~4yD2 2017 09 27.23772 00 59 05.545 +03 04 28.50 22.8z 612582 W84 C~4yD2 2017 10 28.16086 00 56 49.86 +02 50 37.1 612582 G37 C~3cWO 2017 10 28.20697 00 56 49.69 +02 50 36.1 612582 G37 C~3cWO 2017 10 28.29590 00 56 49.29 +02 50 33.9 612582 G37 C~3cWO 2018 09 14.33468 01 04 56.663 +03 41 55.76 23.0i 612582 W84 C~4yD2 2018 09 14.33605 01 04 56.647 +03 41 56.07 24.2g 612582 W84 C~4yD2 2018 09 21.28671 01 04 28.529 +03 38 51.07 23.0z 612582 W84 C~4yD2 2018 10 18.20031 01 02 30.287 +03 26 31.72 23.0z 612582 W84 C~4yD2
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 0.11 0.00 0.20
2 0.0003 0.00 0.23 0.00 0.02
3 0.0242 0.00 -0.60 0.00 -0.10
4 0.0244 0.00 -0.04 0.00 0.27
5 0.1585 0.00 0.00 0.00 -0.02
6 0.1587 0.00 0.14 0.00 -0.05
7 0.9693 0.00 0.03 0.00 -0.08
8 0.9695 0.00 -0.07 0.00 0.08
9 1.1306 0.00 -0.18 0.00 0.04
10 1.1308 0.00 0.40 0.00 -0.20
11 7.0613 0.00 0.12 0.00 -0.04
12 7.0614 0.00 -0.32 0.00 0.12
13 10.1137 0.00 0.07 0.00 -0.30
14 10.1139 0.00 0.06 0.00 -0.06
15 10.1166 0.00 0.17 0.00 0.17
16 10.1352 0.00 0.17 0.00 -0.23
17 10.2473 0.00 0.15 0.00 -0.14
18 10.2474 0.00 0.06 0.00 0.01
19 11.2191 0.00 -0.02 0.00 -0.13
20 11.2220 0.00 -0.14 0.00 -0.00
21 13.0215 0.00 -0.07 0.00 0.17
22 13.0215 0.00 0.01 0.00 -0.11
23 13.1989 0.00 -0.08 0.00 0.08
24 13.1989 0.00 0.00 0.00 -0.13
25 13.2016 0.00 0.12 0.00 0.07
26 14.0096 0.00 0.04 0.00 0.04
27 14.0096 0.00 0.09 0.00 0.22
28 14.0671 0.00 0.07 0.00 -0.05
29 14.0835 0.00 -0.03 0.00 -0.01
30 14.0916 0.00 -0.15 0.00 0.03
31 14.1763 0.00 -0.20 0.00 -0.02
32 14.1764 0.00 0.17 0.00 0.09
33 14.1766 0.00 -0.19 0.00 0.04
34 15.0556 0.00 0.04 0.00 -0.26
35 15.0556 0.00 -0.12 0.00 0.09
36 15.0746 0.00 0.13 0.00 0.27
37 15.1483 0.00 0.01 0.00 0.01
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.
612582 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 43.602 43.602 43.602 ecceobj 0.041 0.041 0.041 incobj 2.950 2.950 2.950 qmin 41.006 41.001 41.006 qmax 45.949 45.948 45.948 amean 43.361 43.361 43.361 amin 43.029 43.029 43.030 amax 43.712 43.712 43.712 emean 0.035 0.035 0.035 emin 0.015 0.015 0.015 emax 0.051 0.051 0.051 imean 1.361 1.361 1.361 imin 0.414 0.414 0.414 imax 2.070 2.070 2.070 excite_mean 0.044 0.044 0.044 fracstop 1.000 1.000 1.000 cjmean 3.092 3.092 3.092 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 169.9 169.9 170.0 kozaiamp 180.0 180.0 180.0