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: 525461
# Created Sun Apr 28 01:08:32 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 55 observations of 55
# Arc: 17.13y
# First observation: 2005/03/11
# Last observation: 2022/04/26
# Chi-squared of fit: 55.92 DOF: 104 RMS: 0.18
# Min/Max residuals: -0.55 0.46
# Exact a, adot, b, bdot, g, gdot:
1.404109E-05 1.902306E-02 -8.833729E-07 -8.290666E-04 2.150148E-02 1.343074E-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
1.825430 -167.555768 0.365395 0.029371 -0.918909 2453440.873943
# Heliocentric elements and errors
Epoch: 2453440.5000 = 2005/03/11
Mean Anomaly: 123.39063 +/- 0.000
Argument of Peri: 13.52370 +/- 0.000
Long of Asc Node: 47.90565 +/- 0.000
Inclination: 3.05023 +/- 0.000
Eccentricity: 0.07892047 +/- 0.0000
Semi-Major Axis: 45.28217057 +/- 0.0000
Time of Perihelion: 2415292.7461 +/- 0.0
Perihelion: 41.70848061 +/- 0.0000
Aphelion: 48.85586054 +/- 0.0000
Period (y) 304.7187 +/- 0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -46.37342114 +/- 0.0000
Ecliptic Y -9.85912502 +/- 0.0000
Ecliptic Z 1.48147946 +/- 0.0000
Ecliptic XDOT 0.00035187 +/- 0.0000
Ecliptic YDOT -0.00241006 +/- 0.0000
Ecliptic ZDOT -0.00010000 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 47.43297805 +/- 0.0000
Geocenter to KBO 46.50842032 +/- 0.0000
# Hcoef: 6.87
The following table shows the complete astrometric record for 525461. 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 (525461) followed by the observatory code and reference code for the source of the astrometry.
2005 03 11.37320 12 48 38.00 -03 14 09.3 23.3R 525461 695 Cn0311 2005 03 11.47546 12 48 37.63 -03 14 07.0 525461 695 Cn0311 2005 03 12.42323 12 48 34.07 -03 13 44.5 525461 695 Cn0311 2005 06 07.04175 12 43 48.04 -02 45 28.7 23.5R 525461 304 Cn6541 2005 06 07.13354 12 43 47.93 -02 45 28.3 525461 304 Cn6541 2005 07 09.97170 12 43 43.39 -02 46 35.0 525461 304 Cn8898 2005 07 10.04704 12 43 43.49 -02 46 35.8 525461 304 Cn8898 2006 04 22.24450 12 49 51.59 -03 25 17.2 23.8R 525461 304 Cr3594 2006 04 22.29782 12 49 51.38 -03 25 15.9 525461 304 Cr3594 2006 04 26.08057 12 49 37.20 -03 23 51.2 23.0R 525461 807 Cr3594 2006 04 26.16378 12 49 36.83 -03 23 49.3 525461 807 Cr3594 2006 04 27.11033 12 49 33.39 -03 23 28.6 525461 807 Cr3594 2006 04 27.17699 12 49 33.12 -03 23 27.8 525461 807 Cr3594 2013 03 12.35916 13 20 01.32 -06 53 39.6 23.4R 525461 695 C~0udE 2013 03 12.43349 13 20 01.07 -06 53 37.6 525461 695 C~0udE 2013 03 13.36292 13 19 57.86 -06 53 18.2 525461 695 C~0udE 2015 02 17.49803 13 28 55.094 -07 53 29.33 23.8r 525461 568 C~2nod 2015 02 17.53937 13 28 55.015 -07 53 28.86 23.6r 525461 568 C~2nod 2015 02 20.47010 13 28 48.897 -07 52 49.97 23.7r 525461 568 C~2nod 2015 03 18.46654 13 27 32.413 -07 45 02.15 23.4r 525461 568 C~2nod 2015 03 18.51775 13 27 32.217 -07 45 01.03 23.7r 525461 568 C~2nod 2015 03 20.51950 13 27 24.995 -07 44 17.85 23.5r 525461 568 C~2nod 2015 03 23.40209 13 27 14.37 -07 43 14.3 23.7R 525461 695 C~1Q3K 2015 03 23.46492 13 27 14.13 -07 43 12.6 525461 695 C~1Q3K 2015 04 11.41033 13 25 59.443 -07 35 54.09 23.4r 525461 568 C~2nod 2015 04 12.36301 13 25 55.587 -07 35 31.54 23.6r 525461 568 C~2nod 2015 04 12.40393 13 25 55.409 -07 35 30.60 23.4r 525461 568 C~2nod 2015 04 12.45094 13 25 55.217 -07 35 29.56 23.4r 525461 568 C~2nod 2015 04 14.46090 13 25 47.044 -07 34 42.26 23.8r 525461 568 C~2nod 2015 04 16.40522 13 25 39.161 -07 33 56.62 23.2r 525461 568 C~2nod 2015 04 18.42156 13 25 30.980 -07 33 09.47 23.5r 525461 568 C~2nod 2015 04 18.46928 13 25 30.787 -07 33 08.22 23.6r 525461 568 C~2nod 2015 05 16.26602 13 23 46.056 -07 23 17.09 23.4r 525461 568 C~2nod 2015 05 25.37165 13 23 17.738 -07 20 43.47 23.7r 525461 568 C~2nod 2015 05 25.41355 13 23 17.616 -07 20 42.73 23.6r 525461 568 C~2nod 2015 05 25.42921 13 23 17.572 -07 20 42.53 23.6r 525461 568 C~2nod 2015 06 22.27832 13 22 21.139 -07 16 01.73 23.7r 525461 568 C~2nod 2015 07 12.27234 13 22 14.318 -07 16 06.39 23.8r 525461 568 C~2nod 2015 07 19.26227 13 22 19.100 -07 16 50.99 23.8r 525461 568 C~2nod 2016 02 04.57138 13 33 08.257 -08 21 46.16 23.9w 525461 568 C~2nod 2016 02 10.55937 13 33 01.302 -08 20 59.16 23.6w 525461 568 C~2nod 2016 02 10.60896 13 33 01.225 -08 20 58.63 23.7w 525461 568 C~2nod 2016 02 11.58117 13 32 59.836 -08 20 49.45 24.0w 525461 568 C~2nod 2016 03 12.48022 13 31 46.233 -08 13 16.45 23.7w 525461 568 C~2nod 2016 04 03.44126 13 30 24.892 -08 05 17.52 23.7w 525461 568 C~2nod 2016 04 09.42106 13 30 00.816 -08 02 58.16 23.9w 525461 568 C~2nod 2017 03 28.57437 13 34 45.374 -08 33 58.93 24.0w 525461 568 C~2nod 2017 03 29.43565 13 34 42.055 -08 33 39.67 23.7w 525461 568 C~2nod 2017 06 24.28972 13 30 04.622 -08 08 26.11 23.8w 525461 568 C~2nod 2018 06 17.01892 13 34 08.50 -08 35 14.3 24.1V 525461 W84 C~30LH 2018 06 17.09033 13 34 08.37 -08 35 13.8 525461 W84 C~30LH 2018 06 17.99261 13 34 06.91 -08 35 06.6 525461 W84 C~30LH 2022 04 26.219980 13 52 33.761 -10 32 07.48 23.5G 525461 G37 C~5aTQ 2022 04 26.271010 13 52 33.572 -10 32 06.53 525461 G37 C~5aTQ 2022 04 26.337750 13 52 33.294 -10 32 04.93 525461 G37 C~5aTQ
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 0.01 0.00 0.06
2 0.0003 0.00 0.22 0.00 -0.09
3 0.0029 0.00 -0.49 0.00 -0.28
4 0.2400 0.00 0.06 0.00 -0.29
5 0.2403 0.00 0.37 0.00 -0.43
6 0.3302 0.00 -0.44 0.00 0.30
7 0.3304 0.00 -0.12 0.00 0.25
8 1.1140 0.00 0.44 0.00 -0.13
9 1.1141 0.00 0.37 0.00 -0.05
10 1.1245 0.00 0.31 0.00 0.27
11 1.1247 0.00 -0.55 0.00 0.35
12 1.1273 0.00 0.02 0.00 0.46
13 1.1275 0.00 -0.30 0.00 -0.18
14 8.0027 0.00 0.18 0.00 -0.22
15 8.0029 0.00 0.33 0.00 0.21
16 8.0054 0.00 0.19 0.00 -0.07
17 9.9387 0.00 -0.12 0.00 -0.00
18 9.9389 0.00 -0.03 0.00 -0.06
19 9.9469 0.00 -0.02 0.00 -0.08
20 10.0181 0.00 -0.03 0.00 -0.03
21 10.0182 0.00 -0.17 0.00 0.00
22 10.0237 0.00 -0.14 0.00 -0.01
23 10.0316 0.00 0.15 0.00 0.15
24 10.0317 0.00 0.13 0.00 0.45
25 10.0836 0.00 -0.14 0.00 -0.01
26 10.0862 0.00 0.00 0.00 0.07
27 10.0863 0.00 -0.13 0.00 0.05
28 10.0865 0.00 -0.09 0.00 -0.02
29 10.0920 0.00 -0.16 0.00 -0.06
30 10.0973 0.00 0.00 0.00 -0.09
31 10.1028 0.00 -0.07 0.00 -0.08
32 10.1029 0.00 -0.01 0.00 0.06
33 10.1790 0.00 0.05 0.00 -0.03
34 10.2040 0.00 -0.04 0.00 -0.06
35 10.2041 0.00 -0.03 0.00 0.03
36 10.2041 0.00 0.00 0.00 -0.01
37 10.2804 0.00 0.05 0.00 -0.01
38 10.3351 0.00 0.04 0.00 -0.04
39 10.3542 0.00 -0.03 0.00 -0.03
40 10.9027 0.00 -0.03 0.00 -0.01
41 10.9191 0.00 -0.01 0.00 -0.17
42 10.9192 0.00 -0.07 0.00 -0.09
43 10.9219 0.00 -0.05 0.00 -0.06
44 11.0037 0.00 -0.04 0.00 0.04
45 11.0638 0.00 -0.02 0.00 0.04
46 11.0802 0.00 -0.10 0.00 -0.01
47 12.0471 0.00 -0.00 0.00 -0.12
48 12.0495 0.00 -0.10 0.00 -0.11
49 12.2872 0.00 0.07 0.00 -0.06
50 13.2667 0.00 0.03 0.00 -0.02
51 13.2669 0.00 -0.06 0.00 -0.07
52 13.2693 0.00 0.10 0.00 0.28
53 17.1248 0.00 -0.15 0.00 0.11
54 17.1250 0.00 0.18 0.00 -0.05
55 17.1252 0.00 0.17 0.00 0.09
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.
525461 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 44.770 44.770 44.770 ecceobj 0.087 0.087 0.087 incobj 3.063 3.063 3.063 qmin 40.238 40.232 40.257 qmax 50.090 50.099 50.080 amean 45.039 45.039 45.039 amin 44.666 44.666 44.667 amax 45.432 45.433 45.432 emean 0.088 0.088 0.088 emin 0.074 0.074 0.074 emax 0.103 0.103 0.103 imean 2.170 2.170 2.170 imin 1.594 1.594 1.594 imax 2.651 2.651 2.651 excite_mean 0.096 0.096 0.096 fracstop 1.000 1.000 1.000 cjmean 3.103 3.103 3.103 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 172.0 172.1 171.8 kozaiamp 180.0 180.0 180.0