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: 612579 # Created Mon Apr 29 01:09:14 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 55 observations of 55 # Arc: 18.05y # First observation: 2003/08/25 # Last observation: 2021/09/12 # Chi-squared of fit: 34.51 DOF: 104 RMS: 0.14 # Min/Max residuals: -0.42 0.42 # Exact a, adot, b, bdot, g, gdot: 1.620025E-05 2.549752E-02 -6.218183E-07 -7.802003E-05 2.504882E-02 1.114353E-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 -0.072242 -12.188542 0.283312 -0.001163 -0.974769 2452876.862803 # Heliocentric elements and errors Epoch: 2452876.5000 = 2003/08/25 Mean Anomaly: 24.78041 +/- 0.000 Argument of Peri: 173.30384 +/- 0.000 Long of Asc Node: 145.19636 +/- 0.000 Inclination: 0.18665 +/- 0.000 Eccentricity: 0.07856509 +/- 0.0000 Semi-Major Axis: 43.97791370 +/- 0.0000 Time of Perihelion: 2445543.9266 +/- 0.0 Perihelion: 40.52278514 +/- 0.0000 Aphelion: 47.43304226 +/- 0.0000 Period (y) 291.6488 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 39.91238795 +/- 0.0000 Ecliptic Y -8.90718359 +/- 0.0000 Ecliptic Z -0.05038642 +/- 0.0000 Ecliptic XDOT 0.00070219 +/- 0.0000 Ecliptic YDOT 0.00269263 +/- 0.0000 Ecliptic ZDOT -0.00000851 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 40.89422101 +/- 0.0000 Geocenter to KBO 39.92203606 +/- 0.0000 # Hcoef: 7.30
The following table shows the complete astrometric record for 612579. 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 (612579) followed by the observatory code and reference code for the source of the astrometry.
2003 08 25.36206 23 15 16.55 -04 53 02.5 22.0R 612579 807 Ci4137 2003 08 26.26631 23 15 12.64 -04 53 27.4 612579 807 Ci4137 2003 08 26.37140 23 15 12.16 -04 53 30.4 612579 807 Ci4137 2003 10 23.17707 23 11 10.86 -05 18 55.9 22.8R 612579 304 Ci9429 2003 10 23.20064 23 11 10.81 -05 18 56.5 612579 304 Ci9429 2004 07 16.37831 23 22 51.53 -04 05 00.9 22.1R 612579 807 Cl4360 2004 07 16.43063 23 22 51.43 -04 05 01.6 612579 807 Cl4360 2004 08 23.15117 23 20 45.80 -04 18 27.5 23.0R 612579 304 Cl4360 2004 08 23.28649 23 20 45.22 -04 18 31.1 612579 304 Cl4360 2008 10 30.240455 23 37 26.22 -02 32 34.2 612579 645 C~1Ghp 2008 10 30.241284 23 37 26.22 -02 32 34.2 612579 645 C~1Ghp 2008 10 30.243772 23 37 26.21 -02 32 34.3 612579 645 C~1Ghp 2013 09 09.19622 00 07 23.652 +00 40 36.47 23.8g 612579 W84 C~4yD1 2013 09 30.16242 00 05 50.38 +00 30 29.5 23.4r 612579 W84 C~3cWO 2013 10 13.06662 00 04 53.977 +00 24 22.89 23.4z 612579 W84 C~4yD1 2013 10 13.10922 00 04 53.79 +00 24 21.6 23.4i 612579 W84 C~3cWO 2013 10 13.10922 00 04 53.794 +00 24 21.60 23.4i 612579 W84 C~4yD1 2013 11 22.06982 00 02 45.35 +00 10 29.8 23.7r 612579 W84 C~3cWO 2013 11 22.06982 00 02 45.352 +00 10 29.84 23.6r 612579 W84 C~4yD1 2013 11 22.07119 00 02 45.344 +00 10 29.57 22.7i 612579 W84 C~4yD1 2013 11 23.08855 00 02 43.494 +00 10 17.72 23.4r 612579 W84 C~4yD1 2014 10 22.16685 00 09 31.68 +00 54 13.5 23.0R 612579 G37 C~1BxD 2014 10 22.27376 00 09 31.26 +00 54 10.8 612579 G37 C~1BxD 2014 10 29.13068 00 09 05.311 +00 51 22.57 23.1z 612579 W84 C~4yD1 2016 10 02.18024 00 21 20.81 +02 10 21.4 22.7i 612579 W84 C~3cWO 2016 10 02.18024 00 21 20.812 +02 10 21.41 22.7i 612579 W84 C~4yD1 2016 10 02.18163 00 21 20.817 +02 10 21.14 22.9r 612579 W84 C~4yD1 2016 10 02.18301 00 21 20.808 +02 10 21.30 24.1g 612579 W84 C~4yD1 2016 11 30.10514 00 18 00.06 +01 48 46.9 23.2i 612579 W84 C~3cWO 2016 12 05.08896 00 17 53.50 +01 48 05.1 23.3r 612579 W84 C~3cWO 2017 08 28.26891 00 29 01.190 +02 59 39.82 24.0r 612579 W84 C~4yD1 2017 08 28.27027 00 29 01.184 +02 59 39.73 24.3g 612579 W84 C~4yD1 2017 09 27.17455 00 26 56.427 +02 46 13.82 22.4z 612579 W84 C~4yD1 2017 10 29.13756 00 24 39.210 +02 31 29.44 22.4z 612579 W84 C~4yD1 2018 09 09.32306 00 33 26.282 +03 27 46.93 22.5i 612579 W84 C~4yD1 2018 09 09.32445 00 33 26.276 +03 27 46.94 23.5r 612579 W84 C~4yD1 2018 09 09.32583 00 33 26.287 +03 27 46.85 23.9g 612579 W84 C~4yD2 2018 10 18.15348 00 30 35.934 +03 09 31.98 22.5z 612579 W84 C~4yD2 2018 10 18.19053 00 30 35.762 +03 09 30.99 22.9i 612579 W84 C~4yD2 2018 11 09.14631 00 29 11.039 +03 00 27.93 23.8r 612579 W84 C~4yD2 2019 11 01.25624 00 34 50.23 +03 36 29.8 24.3g 612579 T09 C~7dBx 2019 11 01.25667 00 34 50.23 +03 36 29.8 24.3g 612579 T09 C~71v6 2019 11 01.30427 00 34 50.03 +03 36 28.8 24.6g 612579 T09 C~7dBx 2019 11 01.30470 00 34 50.03 +03 36 28.8 24.6g 612579 T09 C~71v6 2019 11 01.30637 00 34 50.03 +03 36 28.8 24.2g 612579 T09 C~7dBx 2019 11 01.30680 00 34 50.03 +03 36 28.8 24.2g 612579 T09 C~71v6 2019 11 01.39435 00 34 49.69 +03 36 26.6 24.3g 612579 T09 C~7dBx 2019 11 01.39478 00 34 49.69 +03 36 26.6 24.3g 612579 T09 C~71v6 2019 11 01.41768 00 34 49.59 +03 36 26.0 24.6g 612579 T09 C~7dBx 2019 11 01.41810 00 34 49.59 +03 36 26.0 24.6g 612579 T09 C~71v6 2019 11 01.48448 00 34 49.34 +03 36 24.4 24.5g 612579 T09 C~7dBx 2019 11 01.48491 00 34 49.34 +03 36 24.4 24.5g 612579 T09 C~71v6 2021 09 12.347260 00 48 44.809 +05 04 29.54 23.2G 612579 G37 C~553k 2021 09 12.408180 00 48 44.554 +05 04 28.13 612579 G37 C~553k 2021 09 12.468340 00 48 44.312 +05 04 26.51 612579 G37 C~553k
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 -0.07 0.00 0.10
2 0.0025 0.00 0.18 0.00 0.18
3 0.0028 0.00 -0.04 0.00 0.09
4 0.1610 0.00 -0.13 0.00 0.18
5 0.1611 0.00 0.24 0.00 0.04
6 0.8926 0.00 -0.34 0.00 -0.07
7 0.8927 0.00 -0.11 0.00 -0.05
8 0.9960 0.00 -0.09 0.00 0.15
9 0.9964 0.00 -0.01 0.00 0.22
10 5.1824 0.00 0.12 0.00 -0.39
11 5.1824 0.00 0.15 0.00 -0.37
12 5.1824 0.00 0.12 0.00 -0.42
13 10.0420 0.00 0.42 0.00 -0.14
14 10.0994 0.00 0.04 0.00 0.04
15 10.1347 0.00 -0.02 0.00 0.01
16 10.1348 0.00 -0.03 0.00 -0.11
17 10.1348 0.00 -0.09 0.00 -0.11
18 10.2442 0.00 0.11 0.00 0.10
19 10.2442 0.00 0.08 0.00 0.06
20 10.2442 0.00 0.03 0.00 -0.15
21 10.2470 0.00 0.19 0.00 -0.04
22 11.1589 0.00 -0.42 0.00 0.21
23 11.1592 0.00 -0.27 0.00 0.24
24 11.1780 0.00 0.08 0.00 0.06
25 13.1056 0.00 0.07 0.00 0.06
26 13.1056 0.00 0.04 0.00 0.05
27 13.1056 0.00 0.24 0.00 -0.17
28 13.1056 0.00 0.20 0.00 0.03
29 13.2669 0.00 0.01 0.00 0.09
30 13.2806 0.00 0.04 0.00 0.04
31 14.0093 0.00 -0.05 0.00 0.01
32 14.0093 0.00 -0.06 0.00 -0.05
33 14.0912 0.00 -0.08 0.00 0.07
34 14.1787 0.00 -0.11 0.00 -0.12
35 15.0416 0.00 -0.01 0.00 -0.03
36 15.0416 0.00 -0.02 0.00 0.02
37 15.0417 0.00 0.24 0.00 -0.03
38 15.1480 0.00 0.17 0.00 -0.02
39 15.1481 0.00 0.01 0.00 0.01
40 15.2082 0.00 -0.12 0.00 0.00
41 16.1859 0.00 -0.00 0.00 -0.13
42 16.1859 0.00 0.02 0.00 -0.12
43 16.1860 0.00 -0.19 0.00 0.04
44 16.1860 0.00 -0.17 0.00 0.05
45 16.1860 0.00 -0.07 0.00 0.09
46 16.1860 0.00 -0.04 0.00 0.10
47 16.1863 0.00 -0.02 0.00 0.03
48 16.1863 0.00 0.01 0.00 0.04
49 16.1863 0.00 -0.16 0.00 0.00
50 16.1863 0.00 -0.13 0.00 0.01
51 16.1865 0.00 -0.02 0.00 0.03
52 16.1865 0.00 0.01 0.00 0.04
53 18.0506 0.00 0.07 0.00 -0.03
54 18.0508 0.00 0.02 0.00 0.12
55 18.0509 0.00 0.10 0.00 0.05
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.
612579 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 44.446 44.446 44.446 ecceobj 0.087 0.087 0.087 incobj 0.188 0.188 0.188 qmin 39.843 39.867 39.843 qmax 48.901 48.902 48.900 amean 44.221 44.222 44.221 amin 43.871 43.854 43.874 amax 44.602 44.602 44.601 emean 0.080 0.080 0.080 emin 0.064 0.064 0.064 emax 0.096 0.096 0.096 imean 1.849 1.849 1.849 imin 1.126 1.126 1.126 imax 2.459 2.460 2.459 excite_mean 0.087 0.087 0.087 fracstop 1.000 1.000 1.000 cjmean 3.095 3.095 3.095 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 179.9 179.7 179.9 kozaiamp 180.0 179.9 180.0