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: 527328 # Created Fri Apr 26 01:08:34 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 75 observations of 75 # Arc: 17.31y # First observation: 2000/09/21 # Last observation: 2018/01/12 # Chi-squared of fit: 133.33 DOF: 144 RMS: 0.24 # Min/Max residuals: -0.58 1.62 # Exact a, adot, b, bdot, g, gdot: 2.455421E-05 8.127719E-02 -2.568209E-07 9.739286E-05 5.479573E-02 1.240691E-02 # 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 -3.220905 -23.753183 -0.374050 -0.052227 -0.924466 2451808.703543 # Heliocentric elements and errors Epoch: 2451808.5000 = 2000/09/21 Mean Anomaly: 51.09169 +/- 0.000 Argument of Peri: 201.04765 +/- 0.000 Long of Asc Node: 65.49038 +/- 0.000 Inclination: 3.06593 +/- 0.000 Eccentricity: 0.19218469 +/- 0.0000 Semi-Major Axis: 21.17266253 +/- 0.0000 Time of Perihelion: 2446758.2907 +/- 0.0 Perihelion: 17.10360090 +/- 0.0000 Aphelion: 25.24172416 +/- 0.0000 Period (y) 97.4252 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 17.68104870 +/- 0.0000 Ecliptic Y -7.36501396 +/- 0.0000 Ecliptic Z -1.02534307 +/- 0.0000 Ecliptic XDOT 0.00219506 +/- 0.0000 Ecliptic YDOT 0.00347264 +/- 0.0000 Ecliptic ZDOT -0.00002982 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 19.18101837 +/- 0.0000 Geocenter to KBO 18.24956681 +/- 0.0000 # Hcoef: 9.07
The following table shows the complete astrometric record for 527328. 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 (527328) followed by the observatory code and reference code for the source of the astrometry.
2000 09 21.20280 22 36 54.71 -12 12 41.2 19.0R 527328 695 C~0NlL 2000 09 21.28587 22 36 54.00 -12 12 43.3 527328 695 C~0NlL 2001 09 19.291473 22 54 33.90 -10 25 58.9 22.1V 527328 645 C~1SLI 2001 09 19.292302 22 54 33.89 -10 25 59.0 21.6V 527328 645 C~1SLI 2001 09 19.294790 22 54 33.88 -10 25 59.1 22.5V 527328 645 C~1SLI 2007 09 15.29012 00 27 08.68 -00 05 42.3 22.5 527328 705 cx9534 2007 09 15.29344 00 27 08.66 -00 05 42.3 23.4 527328 705 cx9534 2007 09 22.32252 00 26 10.32 -00 12 01.7 21.5 527328 705 cx9534 2007 09 22.32335 00 26 10.33 -00 12 01.8 21.3 527328 705 cx9534 2007 10 06.33146 00 24 11.32 -00 24 33.2 22.6 527328 705 cx9534 2007 10 06.33395 00 24 11.29 -00 24 33.1 23.5 527328 705 cx9534 2007 10 13.33235 00 23 12.78 -00 30 30.7 22.7 527328 705 cx9534 2007 10 13.33567 00 23 12.78 -00 30 30.8 22.9 527328 705 cx9534 2007 10 15.33725 00 22 56.41 -00 32 09.0 22.4 527328 705 cx9534 2007 10 15.33974 00 22 56.39 -00 32 09.4 23.2 527328 705 cx9534 2007 10 20.32183 00 22 16.69 -00 36 04.9 22.7 527328 705 cx9534 2007 10 20.32515 00 22 16.67 -00 36 04.9 23.5 527328 705 cx9534 2007 11 11.25369 00 19 48.02 -00 49 52.8 22.6 527328 705 cx9534 2007 11 11.25701 00 19 48.01 -00 49 53.0 23.4 527328 705 cx9534 2007 11 12.24062 00 19 42.65 -00 50 20.3 22.6 527328 705 cx9534 2007 11 12.24394 00 19 42.62 -00 50 20.7 23.3 527328 705 cx9534 2008 12 01.09201 00 31 54.85 +00 37 50.3 22.2R 527328 688 C~02eZ 2008 12 01.25939 00 31 54.33 +00 37 49.7 527328 688 C~02eZ 2008 12 21.15619 00 31 30.50 +00 38 14.5 21.4r 527328 695 C~02eZ 2008 12 22.09904 00 31 31.11 +00 38 27.1 21.3r 527328 695 C~02eZ 2008 12 22.18482 00 31 31.17 +00 38 28.2 21.5r 527328 695 C~02eZ 2010 09 17.32927 01 07 09.39 +04 30 54.4 22.2R 527328 688 C~0NHt 2010 09 17.38043 01 07 09.00 +04 30 51.9 527328 688 C~0NHt 2010 10 13.44515 01 03 37.449 +04 09 08.94 22.2G 527328 F51 C~2r7I 2010 10 13.46035 01 03 37.305 +04 09 08.10 22.4G 527328 F51 C~2r7I 2010 10 13.47570 01 03 37.178 +04 09 07.40 22.1G 527328 F51 C~2r7I 2010 10 13.48963 01 03 37.060 +04 09 06.60 22.6G 527328 F51 C~2r7I 2011 09 23.45850 01 19 17.611 +05 53 16.99 22.4G 527328 F51 C~2r7I 2011 09 23.47387 01 19 17.497 +05 53 16.63 22.7G 527328 F51 C~2r7I 2011 09 23.48927 01 19 17.372 +05 53 15.77 22.5G 527328 F51 C~2r7I 2011 09 23.50481 01 19 17.240 +05 53 15.15 22.6G 527328 F51 C~2r7I 2012 10 08.49915 01 29 51.769 +07 04 57.56 22.1G 527328 F51 C~2r7I 2012 10 08.51226 01 29 51.652 +07 04 56.55 22.6G 527328 F51 C~2r7I 2012 10 17.39357 01 28 37.743 +06 57 51.25 22.6G 527328 F51 C~2r7I 2012 10 17.40699 01 28 37.641 +06 57 50.64 22.5G 527328 F51 C~2r7I 2012 10 17.42041 01 28 37.518 +06 57 49.61 23.0G 527328 F51 C~2r7I 2012 10 17.43394 01 28 37.405 +06 57 49.17 22.3G 527328 F51 C~2r7I 2012 11 06.28479 01 25 56.630 +06 42 53.98 22.7G 527328 F51 C~2r7I 2012 11 06.31463 01 25 56.428 +06 42 52.77 22.0G 527328 F51 C~2r7I 2012 11 06.32956 01 25 56.268 +06 42 52.14 22.3G 527328 F51 C~2r7I 2013 10 03.41197 01 43 02.784 +08 30 15.91 22.7G 527328 F51 C~2r7I 2013 10 03.42727 01 43 02.641 +08 30 15.16 22.6G 527328 F51 C~2r7I 2013 10 03.44240 01 43 02.513 +08 30 14.57 22.4G 527328 F51 C~2r7I 2013 10 03.45761 01 43 02.401 +08 30 14.00 22.9G 527328 F51 C~2r7I 2013 11 25.24145 01 36 10.797 +07 53 07.34 22.7G 527328 F51 C~2r7I 2013 11 25.25653 01 36 10.715 +07 53 06.75 22.4G 527328 F51 C~2r7I 2013 11 25.27155 01 36 10.637 +07 53 06.44 22.9G 527328 F51 C~2r7I 2014 08 28.45709 01 58 52.223 +10 08 38.28 23.2G 527328 F51 C~2r7I 2014 09 19.44551 01 56 59.605 +09 57 31.89 22.5G 527328 F51 C~2r7I 2014 10 25.50978 01 52 20.210 +09 31 54.82 22.6G 527328 F51 C~2r7I 2014 10 28.25425 01 51 57.32 +09 29 53.0 22.2R 527328 G37 C~1eNK 2014 10 28.29618 01 51 56.97 +09 29 51.2 527328 G37 C~1eNK 2014 10 28.30824 01 51 56.86 +09 29 50.5 527328 G37 C~1eNK 2015 09 09.46741 02 09 57.367 +11 16 33.54 23.1G 527328 F51 C~2r7I 2015 09 09.47966 02 09 57.300 +11 16 32.95 23.4G 527328 F51 C~2r7I 2015 09 09.49193 02 09 57.236 +11 16 32.79 23.4G 527328 F51 C~2r7I 2015 09 09.50424 02 09 57.170 +11 16 32.58 22.7G 527328 F51 C~2r7I 2015 12 03.24183 01 59 34.968 +10 22 56.23 22.9G 527328 F51 C~2r7I 2015 12 31.30409 01 57 39.724 +10 15 02.95 23.3G 527328 F51 C~2r7I 2016 01 30.25554 01 57 58.048 +10 19 46.50 23.2G 527328 F51 C~2r7I 2016 08 16.53502 02 22 48.671 +12 32 38.15 23.0G 527328 F51 C~2r7I 2016 10 27.31791 02 16 06.643 +11 57 27.76 23.0G 527328 F51 C~2r7I 2016 10 28.54411 02 15 56.337 +11 56 36.52 23.6G 527328 F51 C~2r7I 2016 10 29.52195 02 15 48.137 +11 55 56.45 22.4G 527328 F51 C~2r7I 2016 10 31.34952 02 15 32.853 +11 54 40.73 22.3G 527328 F51 C~2r7I 2017 09 23.47451 02 32 12.035 +13 26 47.73 22.8G 527328 F51 C~2r7I 2017 11 21.42188 02 24 33.642 +12 50 22.91 23.1G 527328 F51 C~2r7I 2017 12 20.14720 02 21 32.165 +12 37 10.19 22.5R 527328 G37 C~2UvC 2017 12 20.22336 02 21 31.816 +12 37 08.77 527328 G37 C~2UvC 2018 01 12.28852 02 20 28.089 +12 33 43.17 21.6G 527328 F51 C~2r7I
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 -0.24 0.00 -0.03
2 0.0002 0.00 -0.12 0.00 1.62
3 0.9941 0.00 0.06 0.00 -0.52
4 0.9941 0.00 0.02 0.00 -0.58
5 0.9941 0.00 0.20 0.00 -0.55
6 6.9818 0.00 0.17 0.00 -0.34
7 6.9818 0.00 0.28 0.00 -0.16
8 7.0010 0.00 -0.08 0.00 0.05
9 7.0010 0.00 0.18 0.00 -0.00
10 7.0394 0.00 0.20 0.00 -0.18
11 7.0394 0.00 0.08 0.00 0.05
12 7.0585 0.00 -0.25 0.00 -0.20
13 7.0585 0.00 0.16 0.00 -0.13
14 7.0640 0.00 -0.04 0.00 0.05
15 7.0640 0.00 -0.03 0.00 -0.23
16 7.0777 0.00 -0.04 0.00 -0.07
17 7.0777 0.00 0.05 0.00 0.09
18 7.1377 0.00 -0.04 0.00 0.04
19 7.1377 0.00 0.09 0.00 -0.07
20 7.1404 0.00 0.10 0.00 -0.05
21 7.1404 0.00 -0.07 0.00 -0.36
22 8.1941 0.00 -0.16 0.00 -0.09
23 8.1945 0.00 -0.28 0.00 1.02
24 8.2490 0.00 -0.01 0.00 0.20
25 8.2516 0.00 0.02 0.00 0.25
26 8.2518 0.00 0.16 0.00 0.15
27 9.9880 0.00 -0.12 0.00 -0.01
28 9.9882 0.00 -0.12 0.00 -0.07
29 10.0595 0.00 0.12 0.00 0.06
30 10.0596 0.00 -0.09 0.00 -0.02
31 10.0596 0.00 -0.03 0.00 0.05
32 10.0596 0.00 -0.02 0.00 -0.06
33 11.0041 0.00 0.01 0.00 -0.16
34 11.0042 0.00 0.10 0.00 0.20
35 11.0042 0.00 0.03 0.00 0.06
36 11.0042 0.00 -0.13 0.00 0.18
37 12.0474 0.00 0.02 0.00 0.21
38 12.0474 0.00 -0.09 0.00 -0.17
39 12.0717 0.00 -0.23 0.00 0.06
40 12.0717 0.00 -0.05 0.00 0.09
41 12.0718 0.00 -0.18 0.00 -0.30
42 12.0718 0.00 -0.14 0.00 -0.10
43 12.1262 0.00 -0.02 0.00 0.15
44 12.1262 0.00 0.43 0.00 0.17
45 12.1263 0.00 -0.22 0.00 0.15
46 13.0327 0.00 0.36 0.00 -0.18
47 13.0328 0.00 0.06 0.00 -0.24
48 13.0328 0.00 -0.04 0.00 -0.15
49 13.0329 0.00 0.12 0.00 -0.03
50 13.1774 0.00 -0.30 0.00 -0.04
51 13.1774 0.00 -0.10 0.00 -0.17
52 13.1775 0.00 0.16 0.00 -0.03
53 13.9336 0.00 0.08 0.00 0.17
54 13.9938 0.00 -0.13 0.00 -0.07
55 14.0926 0.00 0.16 0.00 0.26
56 14.1001 0.00 -0.18 0.00 0.14
57 14.1002 0.00 -0.11 0.00 0.18
58 14.1002 0.00 -0.23 0.00 0.02
59 14.9658 0.00 0.17 0.00 0.11
60 14.9659 0.00 0.08 0.00 -0.14
61 14.9659 0.00 0.04 0.00 0.04
62 14.9659 0.00 -0.02 0.00 0.17
63 15.1979 0.00 -0.04 0.00 0.15
64 15.2747 0.00 0.02 0.00 -0.01
65 15.3567 0.00 -0.09 0.00 0.14
66 15.9023 0.00 -0.01 0.00 0.03
67 16.0989 0.00 -0.15 0.00 0.04
68 16.1022 0.00 -0.02 0.00 -0.35
69 16.1049 0.00 -0.04 0.00 0.07
70 16.1099 0.00 0.16 0.00 -0.17
71 17.0055 0.00 -0.12 0.00 0.08
72 17.1669 0.00 0.10 0.00 -0.01
73 17.2456 0.00 -0.18 0.00 0.05
74 17.2458 0.00 -0.05 0.00 0.03
75 17.3089 0.00 0.63 0.00 -0.44
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.
527328 quality flag:3 Type: CENTAURR CENTAURR CENTAURR axisobj 21.212 21.212 21.212 ecceobj 0.193 0.193 0.193 incobj 3.066 3.066 3.066 qmin 16.838 16.767 16.599 qmax 25.562 25.561 25.563 amean 21.115 21.194 21.099 amin 20.875 20.841 20.696 amax 21.282 21.376 21.283 emean 0.195 0.192 0.196 emin 0.190 0.184 0.190 emax 0.201 0.201 0.201 imean 2.838 2.906 2.576 imin 2.171 2.171 2.171 imax 4.238 3.222 3.114 excite_mean 0.202 0.199 0.201 fracstop 0.001 0.002 0.001 cjmean 3.065 3.064 3.066 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 213.9 231.0 210.1 kozaiamp 16.9 29.5 9.1