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: 525460
# Created Sun Apr 28 01:08:31 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 76 observations of 76
# Arc: 16.96y
# First observation: 2005/03/11
# Last observation: 2022/02/26
# Chi-squared of fit: 69.82 DOF: 146 RMS: 0.17
# Min/Max residuals: -0.47 0.41
# Exact a, adot, b, bdot, g, gdot:
1.403195E-05 2.054521E-02 -3.614012E-07 -7.978768E-04 2.250627E-02 -2.429871E-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
4.315842 146.020152 -0.411157 0.067812 -0.897223 2453440.685363
# Heliocentric elements and errors
Epoch: 2453440.5000 = 2005/03/11
Mean Anomaly: 264.24675 +/- 0.000
Argument of Peri: 226.27804 +/- 0.000
Long of Asc Node: 28.42692 +/- 0.000
Inclination: 4.79328 +/- 0.000
Eccentricity: 0.11197338 +/- 0.0000
Semi-Major Axis: 44.30101306 +/- 0.0000
Time of Perihelion: 2482086.8931 +/- 0.0
Perihelion: 39.34047873 +/- 0.0000
Aphelion: 49.26154738 +/- 0.0000
Period (y) 294.8687 +/- 0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -37.72069080 +/- 0.0000
Ecliptic Y 24.92394308 +/- 0.0000
Ecliptic Z 3.34370160 +/- 0.0000
Ecliptic XDOT -0.00115840 +/- 0.0000
Ecliptic YDOT -0.00224030 +/- 0.0000
Ecliptic ZDOT -0.00011897 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 45.33475720 +/- 0.0000
Geocenter to KBO 44.43217392 +/- 0.0000
# Hcoef: 6.38
The following table shows the complete astrometric record for 525460. 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 (525460) followed by the observatory code and reference code for the source of the astrometry.
2005 03 11.18462 09 59 10.31 +16 54 06.5 22.7R 525460 695 Cn0310 2005 03 12.22712 09 59 06.02 +16 54 25.7 525460 695 Cn0310 2005 03 12.30780 09 59 05.68 +16 54 27.4 525460 695 Cn0310 2005 04 10.17565 09 57 29.32 +17 00 45.0 22.6R 525460 695 Cn3133 2005 04 10.26534 09 57 29.09 +17 00 45.8 525460 695 Cn3133 2005 04 11.18200 09 57 26.92 +17 00 52.0 525460 695 Cn3133 2006 04 27.02138 10 01 30.04 +16 35 02.3 21.6R 525460 807 Cr3594 2006 04 27.13153 10 01 29.90 +16 35 02.4 525460 807 Cr3594 2006 04 28.02385 10 01 28.85 +16 35 02.3 525460 807 Cr3594 2006 12 21.39191 10 13 19.62 +15 29 46.4 22.7R 525460 695 Ct5520 2006 12 21.53327 10 13 19.37 +15 29 48.6 525460 695 Ct5520 2008 04 05.16202 10 11 17.92 +15 37 55.9 21.7R 525460 688 Cy5742 2008 04 05.22354 10 11 17.74 +15 37 56.0 525460 688 Cy5742 2009 02 26.33934 10 18 19.89 +14 57 38.3 23.2R 525460 688 C~04qm 2009 02 26.46299 10 18 19.34 +14 57 41.4 525460 688 C~04qm 2010 05 31.28563 10 19 23.743 +14 40 41.62 22.9G 525460 F51 C~2rXh 2010 06 05.30345 10 19 31.128 +14 39 28.62 22.8G 525460 F51 C~2rXh 2011 03 10.25185 10 26 35.42 +14 03 19.6 21.9R 525460 688 C~0TrZ 2011 03 10.30128 10 26 35.21 +14 03 21.3 525460 688 C~0TrZ 2012 01 21.59644 10 34 30.989 +13 13 20.67 21.2G 525460 F51 C~2rXh 2012 02 03.54494 10 33 41.918 +13 18 35.43 22.7G 525460 F51 C~2rXh 2013 02 09.38198 10 37 47.995 +12 50 43.00 22.6G 525460 F51 C~2rXh 2013 02 09.39692 10 37 47.929 +12 50 43.31 23.4G 525460 F51 C~2rXh 2013 02 09.41207 10 37 47.875 +12 50 43.32 22.1G 525460 F51 C~2rXh 2013 02 09.42723 10 37 47.814 +12 50 43.72 22.2G 525460 F51 C~2rXh 2013 03 03.47194 10 36 10.479 +13 00 12.42 22.6G 525460 F51 C~2rXh 2013 12 04.63181 10 44 50.398 +12 00 45.69 23.1G 525460 F51 C~2rXh 2014 02 26.36247 10 41 08.966 +12 26 51.17 22.5G 525460 F51 C~2rXh 2014 03 06.30029 10 40 33.579 +12 30 12.33 22.6G 525460 F51 C~2rXh 2014 04 04.28413 10 38 36.155 +12 40 22.95 23.5G 525460 F51 C~2rXh 2014 05 21.32664 10 37 09.433 +12 44 36.59 23.4G 525460 F51 C~2rXh 2014 06 17.26829 10 37 40.307 +12 38 51.56 22.5G 525460 F51 C~2rXh 2014 11 27.56500 10 49 12.723 +11 29 38.28 23.3G 525460 F51 C~2rXh 2014 11 29.60186 10 49 14.970 +11 29 35.00 22.9G 525460 F51 C~2rXh 2015 01 20.44037 10 48 12.767 +11 39 35.60 22.4G 525460 F51 C~2rXh 2015 01 20.45380 10 48 12.715 +11 39 35.64 22.7G 525460 F51 C~2rXh 2015 01 20.46722 10 48 12.678 +11 39 35.91 23.1G 525460 F51 C~2rXh 2015 01 20.48062 10 48 12.632 +11 39 36.16 23.0G 525460 F51 C~2rXh 2015 01 22.45259 10 48 06.206 +11 40 20.60 22.8G 525460 F51 C~2rXh 2015 01 22.46616 10 48 06.161 +11 40 20.72 22.5G 525460 F51 C~2rXh 2015 01 22.47982 10 48 06.118 +11 40 21.21 23.1G 525460 F51 C~2rXh 2015 01 22.49357 10 48 06.081 +11 40 21.52 23.1G 525460 F51 C~2rXh 2015 02 16.35180 10 46 29.256 +11 50 46.20 22.1G 525460 F51 C~2rXh 2015 02 16.37690 10 46 29.128 +11 50 46.79 22.4G 525460 F51 C~2rXh 2015 02 17.41661 10 46 24.633 +11 51 14.74 22.2G 525460 F51 C~2rXh 2015 03 15.34784 10 44 30.093 +12 02 15.70 22.6G 525460 F51 C~2rXh 2015 04 10.25291 10 42 50.993 +12 10 38.94 22.8G 525460 F51 C~2rXh 2015 04 10.26486 10 42 50.944 +12 10 38.97 22.6G 525460 F51 C~2rXh 2015 04 10.28908 10 42 50.868 +12 10 39.41 22.6G 525460 F51 C~2rXh 2016 01 09.52692 10 53 16.952 +11 03 51.58 23.4G 525460 F51 C~2rXh 2016 01 19.47768 10 52 50.134 +11 07 09.12 22.2G 525460 F51 C~2rXh 2016 02 09.59008 10 51 33.807 +11 15 39.13 23.0G 525460 F51 C~2rXh 2016 02 11.38584 10 51 26.401 +11 16 26.34 22.7G 525460 F51 C~2rXh 2016 02 11.39751 10 51 26.360 +11 16 26.44 22.4G 525460 F51 C~2rXh 2016 02 11.40913 10 51 26.333 +11 16 26.97 22.8G 525460 F51 C~2rXh 2016 03 06.33263 10 49 41.672 +11 26 58.09 22.4G 525460 F51 C~2rXh 2016 03 06.35602 10 49 41.565 +11 26 59.06 22.8G 525460 F51 C~2rXh 2016 03 06.36774 10 49 41.508 +11 26 59.04 22.9G 525460 F51 C~2rXh 2016 03 10.33466 10 49 23.950 +11 28 38.69 22.8G 525460 F51 C~2rXh 2016 03 13.17818 10 49 11.55 +11 29 48.7 22.3R 525460 G37 C~1pPk 2016 03 13.21858 10 49 11.35 +11 29 49.8 525460 G37 C~1pPk 2016 03 14.13724 10 49 07.37 +11 30 11.8 525460 G37 C~4314 2016 03 14.34004 10 49 06.48 +11 30 16.7 525460 G37 C~4314 2016 03 14.36484 10 49 06.37 +11 30 17.5 525460 G37 C~4314 2016 03 14.39915 10 49 06.23 +11 30 18.1 525460 G37 C~4314 2017 01 27.62212 10 56 55.174 +10 38 06.22 22.8G 525460 F51 C~2rXh 2017 02 21.41855 10 55 15.736 +10 48 47.18 23.0G 525460 F51 C~2rXh 2017 03 05.37764 10 54 22.674 +10 54 04.96 22.4G 525460 F51 C~2rXh 2017 12 28.59718 11 02 42.244 +09 56 05.25 22.7G 525460 F51 C~2rXh 2018 02 12.42269 11 00 30.675 +10 11 50.41 22.7G 525460 F51 C~2rXh 2018 02 12.43441 11 00 30.616 +10 11 50.43 22.6G 525460 F51 C~2rXh 2018 02 12.44626 11 00 30.572 +10 11 50.88 23.2G 525460 F51 C~2rXh 2018 03 19.34088 10 57 58.360 +10 27 06.06 22.7G 525460 F51 C~2rXh 2022 02 26.410405 11 17 54.708 +08 03 19.32 22.3w 525460 F52 C~5V3W 2022 02 26.422586 11 17 54.662 +08 03 19.62 22.3w 525460 F52 C~5V3W 2022 02 26.434876 11 17 54.633 +08 03 19.92 22.1w 525460 F52 C~5V3W
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 -0.07
2 0.0029 0.00 -0.06 0.00 -0.16
3 0.0031 0.00 -0.13 0.00 0.06
4 0.0821 0.00 0.16 0.00 0.02
5 0.0824 0.00 0.08 0.00 0.19
6 0.0849 0.00 0.34 0.00 -0.01
7 1.1275 0.00 0.09 0.00 0.33
8 1.1278 0.00 0.12 0.00 0.41
9 1.1303 0.00 0.08 0.00 0.27
10 1.7802 0.00 0.04 0.00 -0.23
11 1.7806 0.00 0.11 0.00 -0.09
12 3.0691 0.00 -0.32 0.00 0.13
13 3.0692 0.00 -0.19 0.00 -0.47
14 3.9648 0.00 -0.26 0.00 -0.02
15 3.9652 0.00 -0.07 0.00 0.14
16 5.2214 0.00 -0.07 0.00 0.20
17 5.2351 0.00 -0.12 0.00 -0.06
18 5.9961 0.00 -0.29 0.00 -0.32
19 5.9962 0.00 -0.18 0.00 0.26
20 6.8649 0.00 0.01 0.00 0.08
21 6.9004 0.00 -0.04 0.00 -0.29
22 7.9184 0.00 0.01 0.00 0.16
23 7.9184 0.00 -0.01 0.00 0.08
24 7.9185 0.00 0.16 0.00 -0.31
25 7.9185 0.00 0.22 0.00 -0.30
26 7.9789 0.00 -0.01 0.00 0.15
27 8.7350 0.00 -0.03 0.00 0.18
28 8.9642 0.00 -0.27 0.00 0.09
29 8.9859 0.00 0.12 0.00 -0.21
30 9.0653 0.00 0.04 0.00 -0.12
31 9.1941 0.00 -0.19 0.00 -0.02
32 9.2679 0.00 0.32 0.00 -0.07
33 9.7149 0.00 -0.03 0.00 -0.22
34 9.7205 0.00 -0.11 0.00 0.07
35 9.8624 0.00 0.05 0.00 0.29
36 9.8625 0.00 -0.07 0.00 0.03
37 9.8625 0.00 0.03 0.00 0.00
38 9.8625 0.00 -0.01 0.00 -0.05
39 9.8679 0.00 -0.23 0.00 0.03
40 9.8680 0.00 -0.21 0.00 -0.16
41 9.8680 0.00 -0.17 0.00 0.02
42 9.8681 0.00 -0.02 0.00 0.02
43 9.9361 0.00 0.32 0.00 -0.09
44 9.9362 0.00 0.05 0.00 -0.17
45 9.9390 0.00 0.35 0.00 0.23
46 10.0100 0.00 -0.20 0.00 -0.33
47 10.0810 0.00 -0.01 0.00 0.09
48 10.0810 0.00 -0.15 0.00 -0.05
49 10.0811 0.00 -0.10 0.00 0.03
50 10.8319 0.00 -0.03 0.00 0.06
51 10.8591 0.00 0.26 0.00 0.07
52 10.9169 0.00 -0.09 0.00 -0.20
53 10.9218 0.00 -0.33 0.00 -0.02
54 10.9219 0.00 -0.20 0.00 -0.22
55 10.9219 0.00 0.13 0.00 -0.00
56 10.9874 0.00 0.17 0.00 -0.02
57 10.9875 0.00 0.15 0.00 0.35
58 10.9875 0.00 0.09 0.00 0.03
59 10.9984 0.00 -0.19 0.00 -0.25
60 11.0061 0.00 0.35 0.00 0.00
61 11.0063 0.00 0.02 0.00 0.12
62 11.0088 0.00 0.03 0.00 -0.05
63 11.0093 0.00 0.03 0.00 -0.03
64 11.0094 0.00 0.02 0.00 0.18
65 11.0095 0.00 0.17 0.00 -0.04
66 11.8835 0.00 -0.05 0.00 -0.10
67 11.9514 0.00 0.17 0.00 0.12
68 11.9841 0.00 -0.12 0.00 0.00
69 12.8006 0.00 0.10 0.00 0.06
70 12.9260 0.00 -0.03 0.00 0.09
71 12.9261 0.00 -0.18 0.00 -0.20
72 12.9261 0.00 -0.09 0.00 -0.07
73 13.0216 0.00 -0.01 0.00 -0.08
74 16.9643 0.00 -0.16 0.00 0.23
75 16.9644 0.00 -0.04 0.00 0.20
76 16.9644 0.00 0.34 0.00 0.16
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.
525460 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 43.973 43.972 43.973 ecceobj 0.110 0.110 0.110 incobj 4.805 4.805 4.805 qmin 38.648 38.621 38.668 qmax 49.798 49.842 49.793 amean 44.092 44.092 44.092 amin 43.736 43.738 43.741 amax 44.484 44.474 44.490 emean 0.104 0.104 0.104 emin 0.088 0.088 0.088 emax 0.120 0.121 0.120 imean 4.155 4.155 4.155 imin 3.381 3.380 3.381 imax 4.903 4.904 4.903 excite_mean 0.127 0.127 0.127 fracstop 1.000 1.000 1.000 cjmean 3.083 3.083 3.083 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 181.8 181.8 181.8 kozaiamp 180.0 179.9 179.9