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: 10EQ65 # Created Tue Apr 1 01:09:07 2025 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 73 observations of 73 # Arc: 7.21y # First observation: 2010/03/10 # Last observation: 2017/05/27 # Chi-squared of fit: 176.83 DOF: 140 RMS: 0.28 # Min/Max residuals: -0.77 1.28 # Exact a, adot, b, bdot, g, gdot: 2.291437E-05 3.115909E-02 -1.185541E-05 -1.302598E-02 2.789448E-02 4.384989E-03 # Covariance matrix: 1.2254E-13 -5.3877E-14 -1.7871E-14 1.6969E-14 4.9425E-15 -1.8175E-13 -5.3877E-14 4.5765E-14 1.8588E-14 -1.8289E-14 1.2689E-14 1.9475E-13 -1.7871E-14 1.8588E-14 9.0029E-14 -2.2924E-14 3.3948E-15 8.6254E-14 1.6969E-14 -1.8289E-14 -2.2924E-14 1.1704E-14 -5.6062E-15 -8.4756E-14 4.9425E-15 1.2689E-14 3.3948E-15 -5.6062E-15 6.5498E-14 5.5793E-14 -1.8175E-13 1.9475E-13 8.6254E-14 -8.4756E-14 5.5793E-14 9.0271E-13 # lat0 lon0 xBary yBary zBary JD0 -10.481723 -179.214142 0.201755 -0.177674 -0.960484 2455265.556116 # Heliocentric elements and errors Epoch: 2455266.5000 = 2010/03/11 Mean Anomaly: 9.80515 +/- 0.002 Argument of Peri: 180.30962 +/- 0.005 Long of Asc Node: 337.62154 +/- 0.000 Inclination: 24.87496 +/- 0.000 Eccentricity: 0.40121392 +/- 0.0000 Semi-Major Axis: 59.87122031 +/- 0.0045 Time of Perihelion: 2450657.8141 +/- 1.1 Perihelion: 35.85005323 +/- 0.0037 Aphelion: 83.89238738 +/- 0.0068 Period (y) 463.2713 +/- 0.05 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -36.22328360 +/- 0.0003 Ecliptic Y -0.29850328 +/- 0.0000 Ecliptic Z -6.52223750 +/- 0.0001 Ecliptic XDOT -0.00014633 +/- 0.0000 Ecliptic YDOT -0.00305477 +/- 0.0000 Ecliptic ZDOT -0.00133552 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 36.80691245 +/- 0.0003 Geocenter to KBO 35.84931291 +/- 0.0003 # Hcoef: 6.44
The following table shows the complete astrometric record for 10EQ65. 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 (10EQ65) followed by the observatory code and reference code for the source of the astrometry.
2010 03 10.05535 11 46 02.029 -09 55 12.36 21.0R 10EQ65 809 C~0F7m 2010 03 10.13852 11 46 01.662 -09 55 10.92 21.4R 10EQ65 809 C~0F7m 2010 03 10.22179 11 46 01.194 -09 55 10.05 21.5R 10EQ65 809 C~0F7m 2010 03 11.13741 11 45 56.393 -09 54 49.17 22.1R 10EQ65 809 C~0F7m 2010 03 11.22125 11 45 55.931 -09 54 46.94 21.5R 10EQ65 809 C~0F7m 2010 03 12.26475 11 45 50.454 -09 54 24.04 10EQ65 807 C~0F7m 2010 03 12.31187 11 45 50.200 -09 54 22.72 10EQ65 807 C~0F7m 2010 03 13.22443 11 45 45.382 -09 54 01.75 21.7R 10EQ65 807 C~0F7m 2010 03 13.24310 11 45 45.276 -09 54 01.58 21.7R 10EQ65 807 C~0F7m 2010 03 13.46604 11 45 44.099 -09 53 57.49 22.0r 10EQ65 F51 C~1w3h 2010 03 26.20104 11 44 36.933 -09 48 32.88 21.5R 10EQ65 807 C~0Fo2 2010 03 26.23750 11 44 36.744 -09 48 31.44 21.5R 10EQ65 807 C~0Fo2 2010 04 20.25828 11 42 36.93 -09 36 32.9 22.0R 10EQ65 688 C~0GX1 2010 04 20.30377 11 42 36.74 -09 36 31.6 10EQ65 688 C~0GX1 2010 05 17.27329 11 41 10.530 -09 24 54.86 21.2z 10EQ65 F51 C~1w3h 2010 05 17.28519 11 41 10.492 -09 24 54.74 21.3z 10EQ65 F51 C~1w3h 2011 03 25.35488 11 50 06.491 -11 12 48.35 21.8r 10EQ65 F51 C~1w3h 2011 03 25.37768 11 50 06.365 -11 12 47.22 21.7i 10EQ65 F51 C~1w3h 2011 03 25.38932 11 50 06.293 -11 12 47.06 21.7i 10EQ65 F51 C~1w3h 2011 05 19.27344 11 46 26.187 -10 47 19.91 21.1G 10EQ65 F51 C~2rXn 2011 05 19.28414 11 46 26.179 -10 47 19.14 21.8G 10EQ65 F51 C~2rXn 2012 01 08.58792 12 00 23.919 -12 41 16.55 21.1z 10EQ65 F51 C~1w3h 2012 01 08.64665 12 00 23.850 -12 41 17.98 21.8G 10EQ65 F51 C~2rXn 2012 03 16.51575 11 56 13.337 -12 38 47.65 21.7i 10EQ65 F51 C~1w3h 2012 03 16.52849 11 56 13.262 -12 38 47.09 22.1i 10EQ65 F51 C~1w3h 2012 04 13.34782 11 53 51.253 -12 26 02.10 22.1w 10EQ65 F51 C~1w3h 2012 04 13.36105 11 53 51.184 -12 26 01.67 22.0w 10EQ65 F51 C~1w3i 2012 04 13.37430 11 53 51.120 -12 26 01.31 21.9w 10EQ65 F51 C~1w3i 2012 04 13.38753 11 53 51.056 -12 26 00.80 22.0w 10EQ65 F51 C~1w3i 2013 01 08.64212 12 05 41.641 -14 01 02.50 20.8z 10EQ65 F51 C~1w3i 2013 01 08.64406 12 05 41.617 -14 01 02.62 22.1G 10EQ65 F51 C~2rXn 2013 03 04.50390 12 02 41.518 -14 04 06.38 21.9r 10EQ65 F51 C~1w3i 2013 03 04.51534 12 02 41.478 -14 04 05.97 21.4i 10EQ65 F51 C~1w3i 2013 03 04.52746 12 02 41.407 -14 04 05.95 21.3i 10EQ65 F51 C~1w3i 2014 01 01.64604 12 11 03.554 -15 15 51.22 22.6G 10EQ65 F51 C~2rXn 2014 01 17.64055 12 10 50.536 -15 22 33.01 22.3G 10EQ65 F51 C~2rXn 2014 04 05.37640 12 05 22.432 -15 12 06.77 21.9w 10EQ65 F51 C~1w3i 2014 04 05.38760 12 05 22.379 -15 12 06.62 22.1w 10EQ65 F51 C~1w3i 2014 04 05.39884 12 05 22.310 -15 12 06.04 22.1w 10EQ65 F51 C~1w3i 2014 04 05.41006 12 05 22.271 -15 12 05.74 22.1w 10EQ65 F51 C~1w3i 2014 05 25.27911 12 02 14.291 -14 47 31.20 22.3G 10EQ65 F51 C~2rXn 2014 05 25.29124 12 02 14.264 -14 47 30.80 22.6G 10EQ65 F51 C~2rXn 2014 05 25.30333 12 02 14.239 -14 47 30.36 22.6G 10EQ65 F51 C~2rXn 2014 05 25.31541 12 02 14.223 -14 47 30.35 22.3G 10EQ65 F51 C~2rXn 2015 01 28.56355 12 15 50.594 -16 42 48.76 22.2G 10EQ65 F51 C~2rXn 2015 01 28.57543 12 15 50.556 -16 42 48.94 22.3G 10EQ65 F51 C~2rXn 2015 01 28.58733 12 15 50.525 -16 42 49.14 22.3G 10EQ65 F51 C~2rXn 2015 01 28.59921 12 15 50.494 -16 42 49.22 22.5G 10EQ65 F51 C~2rXn 2016 01 10.66233 12 21 41.576 -17 52 21.02 22.3G 10EQ65 F51 C~2rXn 2016 02 20.52138 12 19 58.484 -18 01 22.15 22.7G 10EQ65 F51 C~2rXn 2016 03 03.45105 12 19 04.421 -18 00 01.14 22.4G 10EQ65 F51 C~2rXn 2016 03 04.48751 12 18 59.406 -17 59 49.19 21.9G 10EQ65 F51 C~2rXn 2016 03 04.49866 12 18 59.348 -17 59 49.36 22.6G 10EQ65 F51 C~2rXn 2016 03 04.50989 12 18 59.305 -17 59 49.13 22.3G 10EQ65 F51 C~2rXn 2016 03 04.52101 12 18 59.236 -17 59 48.93 21.8G 10EQ65 F51 C~2rXn 2016 06 05.26838 12 12 40.291 -17 18 33.13 23.1G 10EQ65 F51 C~2rXn 2016 06 05.27873 12 12 40.271 -17 18 32.90 23.0G 10EQ65 F51 C~2rXn 2016 06 05.28914 12 12 40.275 -17 18 32.45 23.2G 10EQ65 F51 C~2rXn 2016 06 05.29950 12 12 40.259 -17 18 32.63 22.4G 10EQ65 F51 C~2rXn 2017 03 05.47437 12 24 24.159 -19 15 30.82 22.0G 10EQ65 F51 C~2rXn 2017 03 05.48571 12 24 24.086 -19 15 30.67 22.7G 10EQ65 F51 C~2rXn 2017 03 05.49706 12 24 24.037 -19 15 30.37 23.0G 10EQ65 F51 C~2rXn 2017 03 05.50844 12 24 23.984 -19 15 30.35 21.9G 10EQ65 F51 C~2rXn 2017 03 17.52139 12 23 23.273 -19 12 34.47 21.5G 10EQ65 F51 C~2rXn 2017 03 25.46965 12 22 41.439 -19 09 50.84 22.5G 10EQ65 F51 C~2rXn 2017 03 25.48011 12 22 41.373 -19 09 50.55 22.5G 10EQ65 F51 C~2rXn 2017 03 25.49056 12 22 41.297 -19 09 50.29 22.3G 10EQ65 F51 C~2rXn 2017 03 25.50102 12 22 41.256 -19 09 50.26 21.8G 10EQ65 F51 C~2rXn 2017 04 15.42286 12 20 52.798 -19 00 23.18 22.2G 10EQ65 F51 C~2rXn 2017 05 27.26450 12 18 17.973 -18 38 28.34 22.3G 10EQ65 F51 C~2rXn 2017 05 27.27553 12 18 17.957 -18 38 27.97 21.9G 10EQ65 F51 C~2rXn 2017 05 27.28653 12 18 17.938 -18 38 27.65 22.7G 10EQ65 F51 C~2rXn 2017 05 27.29755 12 18 17.898 -18 38 27.24 21.6G 10EQ65 F51 C~2rXn
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 -0.63 0.00 1.28
2 0.0002 0.00 0.49 0.00 0.91
3 0.0005 0.00 0.14 0.00 -0.04
4 0.0030 0.00 0.20 0.00 0.53
5 0.0032 0.00 0.00 0.00 0.89
6 0.0060 0.00 0.37 0.00 0.19
7 0.0062 0.00 0.35 0.00 0.43
8 0.0087 0.00 0.22 0.00 0.38
9 0.0087 0.00 0.14 0.00 0.12
10 0.0093 0.00 0.13 0.00 -0.77
11 0.0442 0.00 0.06 0.00 -0.63
12 0.0443 0.00 0.12 0.00 -0.19
13 0.1128 0.00 0.01 0.00 -0.17
14 0.1129 0.00 0.07 0.00 -0.18
15 0.1868 0.00 -0.05 0.00 -0.08
16 0.1868 0.00 -0.23 0.00 -0.22
17 1.0412 0.00 0.15 0.00 -0.55
18 1.0413 0.00 0.09 0.00 -0.02
19 1.0413 0.00 -0.06 0.00 -0.17
20 1.1916 0.00 -0.73 0.00 -0.66
21 1.1916 0.00 -0.51 0.00 -0.14
22 1.8331 0.00 0.16 0.00 -0.06
23 1.8332 0.00 0.05 0.00 -0.18
24 2.0191 0.00 -0.08 0.00 -0.30
25 2.0191 0.00 -0.18 0.00 -0.04
26 2.0953 0.00 0.30 0.00 -0.42
27 2.0953 0.00 0.21 0.00 -0.39
28 2.0953 0.00 0.20 0.00 -0.42
29 2.0954 0.00 0.19 0.00 -0.31
30 2.8353 0.00 -0.28 0.00 0.25
31 2.8353 0.00 -0.61 0.00 0.18
32 2.9855 0.00 -0.25 0.00 -0.19
33 2.9855 0.00 0.02 0.00 0.04
34 2.9855 0.00 -0.11 0.00 -0.13
35 3.8154 0.00 -0.06 0.00 -0.34
36 3.8592 0.00 -0.16 0.00 -0.15
37 4.0721 0.00 0.04 0.00 0.07
38 4.0721 0.00 0.12 0.00 -0.11
39 4.0721 0.00 -0.04 0.00 0.15
40 4.0722 0.00 0.25 0.00 0.13
41 4.2087 0.00 -0.14 0.00 -0.02
42 4.2087 0.00 -0.19 0.00 0.07
43 4.2088 0.00 -0.21 0.00 0.21
44 4.2088 0.00 -0.09 0.00 -0.08
45 4.8885 0.00 0.05 0.00 0.07
46 4.8885 0.00 -0.05 0.00 0.04
47 4.8885 0.00 -0.05 0.00 -0.00
48 4.8886 0.00 -0.05 0.00 0.08
49 5.8388 0.00 -0.13 0.00 0.12
50 5.9506 0.00 0.05 0.00 -0.07
51 5.9833 0.00 -0.28 0.00 0.02
52 5.9861 0.00 -0.04 0.00 0.23
53 5.9862 0.00 -0.08 0.00 -0.08
54 5.9862 0.00 0.11 0.00 0.02
55 5.9862 0.00 -0.10 0.00 0.09
56 6.2401 0.00 -0.11 0.00 0.18
57 6.2402 0.00 -0.22 0.00 0.17
58 6.2402 0.00 0.02 0.00 0.38
59 6.2402 0.00 -0.04 0.00 -0.04
60 6.9881 0.00 0.25 0.00 -0.06
61 6.9882 0.00 -0.01 0.00 -0.03
62 6.9882 0.00 0.10 0.00 0.15
63 6.9882 0.00 0.15 0.00 0.05
64 7.0211 0.00 -0.01 0.00 0.03
65 7.0429 0.00 0.33 0.00 -0.07
66 7.0429 0.00 0.19 0.00 -0.02
67 7.0429 0.00 -0.11 0.00 -0.00
68 7.0430 0.00 0.13 0.00 -0.21
69 7.1003 0.00 0.17 0.00 -0.21
70 7.2148 0.00 -0.04 0.00 0.01
71 7.2148 0.00 0.09 0.00 0.06
72 7.2149 0.00 0.16 0.00 0.07
73 7.2149 0.00 -0.08 0.00 0.17
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.
10EQ65 quality flag:3 Type: SCATNEAR SCATNEAR SCATNEAR axisobj 59.903 59.903 59.903 ecceobj 0.402 0.402 0.402 incobj 24.866 24.866 24.866 qmin 35.339 35.248 35.341 qmax 86.468 86.529 86.427 amean 60.287 60.287 60.287 amin 59.588 59.589 59.597 amax 61.208 61.179 61.186 emean 0.404 0.404 0.404 emin 0.394 0.395 0.394 emax 0.413 0.415 0.413 imean 25.897 25.886 25.900 imin 25.677 25.626 25.662 imax 26.097 26.111 26.101 excite_mean 0.595 0.595 0.595 fracstop 1.000 1.000 1.000 cjmean 2.828 2.828 2.828 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 178.1 178.9 177.4 kozaiamp 180.0 180.0 180.0