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: 10EU65
# Created Fri Nov 22 02:09:05 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 51 observations of 51
# Arc: 10.12y
# First observation: 2009/04/21
# Last observation: 2019/06/06
# Chi-squared of fit: 191.90 DOF: 96 RMS: 0.34
# Min/Max residuals: -0.91 0.93
# Exact a, adot, b, bdot, g, gdot:
2.085415E-05 8.411409E-02 -4.853335E-06 -2.186146E-02 5.744459E-02 -1.300627E-02
# Covariance matrix:
1.1388E-13 -4.0875E-14 -7.7629E-15 6.3238E-15 -8.8938E-14 -1.5585E-14
-4.0875E-14 2.3638E-14 5.7424E-15 -4.7453E-15 2.5747E-14 1.4790E-14
-7.7629E-15 5.7424E-15 5.0789E-14 -1.1077E-14 3.3091E-15 4.9784E-15
6.3238E-15 -4.7453E-15 -1.1077E-14 5.1166E-15 -2.4485E-15 -4.1604E-15
-8.8938E-14 2.5747E-14 3.3091E-15 -2.4485E-15 1.8476E-13 -5.3154E-15
-1.5585E-14 1.4790E-14 4.9784E-15 -4.1604E-15 -5.3154E-15 1.5073E-14
# lat0 lon0 xBary yBary zBary JD0
0.909969 179.625381 -0.519848 0.013654 -0.860200 2454942.657056
# Heliocentric elements and errors
Epoch: 2454942.5000 = 2009/04/21
Mean Anomaly: 310.93073 +/- 0.006
Argument of Peri: 239.83904 +/- 0.007
Long of Asc Node: 4.60353 +/- 0.000
Inclination: 14.58249 +/- 0.000
Eccentricity: 0.14617866 +/- 0.0000
Semi-Major Axis: 19.89916675 +/- 0.0006
Time of Perihelion: 2459361.8447 +/- 1.4
Perihelion: 16.99033319 +/- 0.0006
Aphelion: 22.80800031 +/- 0.0008
Period (y) 88.7688 +/- 0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -18.26649694 +/- 0.0001
Ecliptic Y -0.40491675 +/- 0.0000
Ecliptic Z 0.27640501 +/- 0.0000
Ecliptic XDOT 0.00058212 +/- 0.0000
Ecliptic YDOT -0.00400901 +/- 0.0000
Ecliptic ZDOT -0.00105175 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 18.27312572 +/- 0.0001
Geocenter to KBO 17.40818018 +/- 0.0001
# Hcoef: 9.08
The following table shows the complete astrometric record for 10EU65. 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 (10EU65) followed by the observatory code and reference code for the source of the astrometry.
2009 04 21.15629 12 00 04.39 +00 59 02.0 21.2V 10EU65 G96 C~3xq1 2009 04 21.16446 12 00 04.28 +00 59 02.2 22.2V 10EU65 G96 C~3xq1 2009 04 21.17267 12 00 04.17 +00 59 02.4 21.0V 10EU65 G96 C~3xq1 2009 04 21.18081 12 00 04.14 +00 59 02.7 21.4V 10EU65 G96 C~3xq1 2010 02 15.47787 12 25 56.02 -02 56 43.3 22.1g 10EU65 F51 C~3xq1 2010 02 15.48621 12 25 55.97 -02 56 43.2 10EU65 F51 C~3xq1 2010 03 13.08329 12 22 18.303 -02 39 17.67 21.2R 10EU65 809 C~0F7n 2010 03 13.16817 12 22 17.516 -02 39 13.50 21.3R 10EU65 809 C~0F7n 2010 03 13.25226 12 22 16.717 -02 39 09.79 21.8R 10EU65 809 C~0F7n 2010 03 14.16396 12 22 07.841 -02 38 24.75 21.2R 10EU65 809 C~0F7n 2010 03 14.24839 12 22 06.987 -02 38 22.02 21.3R 10EU65 809 C~0F7n 2010 03 16.22843 12 21 47.541 -02 36 42.75 21.4R 10EU65 807 C~0F7n 2010 03 16.25617 12 21 47.271 -02 36 41.57 21.5R 10EU65 807 C~0F7n 2010 03 18.07817 12 21 29.279 -02 35 11.00 21.5R 10EU65 809 C~0Fo2 2010 03 18.16131 12 21 28.440 -02 35 06.79 21.0R 10EU65 809 C~0Fo2 2010 03 18.24527 12 21 27.616 -02 35 02.72 21.4R 10EU65 809 C~0Fo2 2010 03 20.07412 12 21 09.397 -02 33 30.49 21.2R 10EU65 809 C~0Fo2 2010 03 20.15781 12 21 08.562 -02 33 25.84 21.2R 10EU65 809 C~0Fo2 2010 03 20.24245 12 21 07.709 -02 33 22.06 21.3R 10EU65 809 C~0Fo2 2010 03 21.07089 12 20 59.410 -02 32 40.05 21.0R 10EU65 809 C~0Fo2 2010 03 21.15458 12 20 58.594 -02 32 35.91 21.4R 10EU65 809 C~0Fo2 2010 03 21.23733 12 20 57.733 -02 32 31.38 21.8R 10EU65 809 C~0Fo2 2010 03 22.06794 12 20 49.490 -02 31 49.36 21.0R 10EU65 809 C~0Fo2 2010 03 22.15139 12 20 48.574 -02 31 45.33 21.0R 10EU65 809 C~0Fo2 2010 03 22.23561 12 20 47.747 -02 31 40.40 21.5R 10EU65 809 C~0Fo2 2010 03 27.20981 12 19 57.673 -02 27 27.27 21.2R 10EU65 807 C~0Fo2 2010 03 27.26098 12 19 57.164 -02 27 24.19 21.2R 10EU65 807 C~0Fo2 2010 04 17.40060 12 16 31.44 -02 10 00.9 10EU65 F51 C~3xq1 2010 04 17.40980 12 16 31.35 -02 10 00.6 10EU65 F51 C~3xq1 2010 04 21.09270 12 15 58.608 -02 07 16.66 21.8R 10EU65 807 C~0Gty 2010 04 21.15461 12 15 58.075 -02 07 13.98 21.5R 10EU65 807 C~0Gty 2010 05 13.30326 12 13 16.02 -01 54 28.2 10EU65 F51 C~3xq1 2010 05 13.31516 12 13 15.94 -01 54 27.8 10EU65 F51 C~3xq1 2010 06 03.00167 12 11 56.614 -01 50 01.64 21.2R 10EU65 807 C~0IRj 2010 06 06.02025 12 11 51.702 -01 50 05.61 21.5R 10EU65 807 C~0IRj 2010 06 06.09407 12 11 51.622 -01 50 06.06 21.2R 10EU65 807 C~0IRj 2013 04 16.243843 13 07 17.22 -11 47 08.0 21.3r 10EU65 W84 C~3xq1 2013 04 16.264155 13 07 17.00 -11 47 07.0 10EU65 W84 C~3xq1 2013 04 16.269676 13 07 16.95 -11 47 06.7 21.4r 10EU65 W84 C~3xq1 2013 04 16.300914 13 07 16.62 -11 47 05.1 10EU65 W84 C~3xq1 2013 04 16.305046 13 07 16.58 -11 47 04.9 10EU65 W84 C~3xq1 2013 04 16.309410 13 07 16.53 -11 47 04.7 21.3r 10EU65 W84 C~3xq1 2013 04 16.313565 13 07 16.48 -11 47 04.5 10EU65 W84 C~3xq1 2013 04 17.148947 13 07 07.87 -11 46 22.4 21.4r 10EU65 W84 C~3xq1 2013 04 17.153137 13 07 07.83 -11 46 22.2 21.5r 10EU65 W84 C~3xq1 2013 04 17.157280 13 07 07.78 -11 46 22.0 21.4r 10EU65 W84 C~3xq2 2013 04 17.161470 13 07 07.73 -11 46 21.8 21.4r 10EU65 W84 C~3xq2 2015 08 02.037859 13 36 41.48 -17 20 06.3 10EU65 W84 C~3xq2 2015 08 02.038553 13 36 41.49 -17 20 06.4 21.4i 10EU65 W84 C~3xq2 2015 09 01.014063 13 41 06.57 -17 39 53.3 21.4i 10EU65 W84 C~43wZ 2019 06 06.185243 15 01 34.68 -29 12 18.6 10EU65 W84 C~43wZ
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 0.34 0.00 -0.41
2 0.0000 0.00 -0.29 0.00 -0.52
3 0.0000 0.00 -0.91 0.00 -0.63
4 0.0001 0.00 -0.35 0.00 -0.64
5 0.8222 0.00 -0.36 0.00 0.18
6 0.8223 0.00 -0.22 0.00 0.02
7 0.8923 0.00 -0.25 0.00 0.35
8 0.8926 0.00 0.46 0.00 0.40
9 0.8928 0.00 0.93 0.00 0.03
10 0.8953 0.00 0.54 0.00 0.60
11 0.8955 0.00 0.31 0.00 -0.80
12 0.9010 0.00 -0.23 0.00 0.82
13 0.9010 0.00 -0.11 0.00 0.62
14 0.9060 0.00 -0.10 0.00 0.27
15 0.9062 0.00 -0.11 0.00 0.31
16 0.9065 0.00 0.27 0.00 0.17
17 0.9115 0.00 -0.12 0.00 0.22
18 0.9117 0.00 0.08 0.00 0.65
19 0.9119 0.00 0.21 0.00 0.14
20 0.9142 0.00 -0.36 0.00 0.14
21 0.9144 0.00 0.16 0.00 0.04
22 0.9147 0.00 -0.09 0.00 0.37
23 0.9169 0.00 0.78 0.00 0.14
24 0.9172 0.00 -0.21 0.00 -0.08
25 0.9174 0.00 0.30 0.00 0.56
26 0.9310 0.00 0.12 0.00 -0.81
27 0.9312 0.00 0.36 0.00 -0.35
28 0.9890 0.00 -0.35 0.00 -0.08
29 0.9891 0.00 -0.42 0.00 -0.20
30 0.9991 0.00 0.14 0.00 -0.24
31 0.9993 0.00 0.41 0.00 -0.23
32 1.0600 0.00 -0.20 0.00 -0.19
33 1.0600 0.00 -0.35 0.00 -0.08
34 1.1166 0.00 0.60 0.00 0.38
35 1.1249 0.00 -0.21 0.00 0.17
36 1.1251 0.00 0.22 0.00 -0.05
37 3.9866 0.00 -0.07 0.00 -0.12
38 3.9866 0.00 -0.15 0.00 -0.15
39 3.9866 0.00 -0.03 0.00 -0.13
40 3.9867 0.00 -0.05 0.00 -0.12
41 3.9867 0.00 -0.00 0.00 -0.13
42 3.9867 0.00 -0.06 0.00 -0.15
43 3.9867 0.00 -0.16 0.00 -0.16
44 3.9890 0.00 -0.03 0.00 -0.19
45 3.9890 0.00 0.03 0.00 -0.20
46 3.9891 0.00 -0.06 0.00 -0.21
47 3.9891 0.00 -0.15 0.00 -0.23
48 6.2803 0.00 -0.19 0.00 0.10
49 6.2803 0.00 -0.10 0.00 0.01
50 6.3624 0.00 -0.01 0.00 0.04
51 10.1247 0.00 0.26 0.00 0.38
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.
10EU65 quality flag:3 Type: CENTAURR CENTAURR CENTAURR axisobj 19.893 19.893 19.893 ecceobj 0.144 0.143 0.144 incobj 14.587 14.587 14.587 qmin 16.121 17.037 17.038 qmax 25.593 23.715 24.105 amean 20.782 20.200 20.305 amin 19.893 19.893 19.756 amax 21.228 20.435 21.025 emean 0.193 0.152 0.142 emin 0.144 0.141 0.116 emax 0.223 0.161 0.166 imean 13.912 15.154 15.838 imin 12.505 14.926 14.923 imax 15.624 15.481 16.572 excite_mean 0.309 0.303 0.308 fracstop 0.020 0.001 0.006 cjmean 3.031 3.048 3.043 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 188.7 240.0 259.3 kozaiamp 179.6 5.3 17.6