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: 10VE253
# Created Tue Apr 23 01:13:35 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 73 observations of 73
# Arc: 11.42y
# First observation: 2009/09/15
# Last observation: 2021/02/15
# Chi-squared of fit: 65.80 DOF: 140 RMS: 0.17
# Min/Max residuals: -0.51 0.42
# Exact a, adot, b, bdot, g, gdot:
2.917584E-05 1.185982E-01 4.307686E-06 1.192835E-02 6.354577E-02 -4.215791E-03
# Covariance matrix:
1.1796E-13 -3.0450E-14 3.5438E-15 -1.9604E-15 2.1720E-14 -1.5272E-14
-3.0450E-14 2.0380E-14 -3.1528E-15 1.7427E-15 2.1718E-14 6.2356E-15
3.5438E-15 -3.1528E-15 7.0087E-14 -1.2097E-14 -3.6185E-15 -1.1779E-15
-1.9604E-15 1.7427E-15 -1.2097E-14 3.0344E-15 1.9978E-15 6.5154E-16
2.1720E-14 2.1718E-14 -3.6185E-15 1.9978E-15 9.7422E-14 -5.8289E-15
-1.5272E-14 6.2356E-15 -1.1779E-15 6.5154E-16 -5.8289E-15 4.8271E-15
# lat0 lon0 xBary yBary zBary JD0
5.529207 25.244831 0.535798 0.081561 -0.842518 2455090.090560
# Heliocentric elements and errors
Epoch: 2455090.5000 = 2009/09/16
Mean Anomaly: 356.41673 +/- 309.620
Argument of Peri: 53.52894 +/- 0.000
Long of Asc Node: 341.90053 +/- 0.000
Inclination: 7.89090 +/- 0.000
Eccentricity: 0.48549978 +/- 0.0000
Semi-Major Axis: 32.02219745 +/- 0.2245
Time of Perihelion: 2455749.2977 +/- 56929.0
Perihelion: 16.47542754 +/- 0.1155
Aphelion: 47.56896735 +/- 0.3335
Period (y) 181.2111 +/- 1.91
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X 15.16480879 +/- 0.0000
Ecliptic Y 6.55356698 +/- 0.0000
Ecliptic Z 1.51634884 +/- 0.0000
Ecliptic XDOT -0.00238367 +/- 0.0000
Ecliptic YDOT 0.00452851 +/- 0.0000
Ecliptic ZDOT 0.00049396 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 16.58978635 +/- 0.0000
Geocenter to KBO 15.73673463 +/- 0.0000
# Hcoef: 9.97
The following table shows the complete astrometric record for 10VE253. 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 (10VE253) followed by the observatory code and reference code for the source of the astrometry.
2009 09 15.589794 01 25 13.857 +14 54 27.11 22.0G 10VE253 F51 C~434g 2009 09 15.600215 01 25 13.746 +14 54 26.88 21.8G 10VE253 F51 C~434g 2010 07 17.577535 01 52 14.979 +17 39 45.06 22.5G 10VE253 F51 C~434g 2010 07 19.553922 01 52 25.009 +17 41 35.22 22.0G 10VE253 F51 C~434g 2010 07 19.562658 01 52 25.052 +17 41 35.10 22.1G 10VE253 F51 C~434g 2010 10 03.539185 01 48 10.986 +17 51 04.01 21.8G 10VE253 F51 C~434g 2010 10 03.550193 01 48 10.849 +17 51 03.54 22.3G 10VE253 F51 C~434g 2010 10 07.390432 01 47 32.323 +17 48 30.97 22.0G 10VE253 F51 C~434g 2010 10 07.405817 01 47 32.169 +17 48 30.41 21.7G 10VE253 F51 C~434g 2010 10 07.422240 01 47 31.996 +17 48 29.75 22.2G 10VE253 F51 C~434g 2010 10 07.439314 01 47 31.819 +17 48 29.08 21.8G 10VE253 F51 C~434g 2010 10 30.292280 01 43 30.088 +17 29 43.26 22.0G 10VE253 F51 C~434g 2010 11 02.23514 01 42 59.29 +17 27 01.0 22.7V 10VE253 G96 C~434g 2010 11 02.24350 01 42 59.18 +17 27 00.1 21.2V 10VE253 G96 C~434g 2010 11 02.25174 01 42 59.07 +17 27 00.0 21.4V 10VE253 G96 C~434g 2010 11 02.26001 01 42 59.00 +17 26 59.4 21.7V 10VE253 G96 C~434g 2010 11 03.437089 01 42 46.820 +17 25 54.15 22.1G 10VE253 F51 C~434g 2010 11 03.462741 01 42 46.561 +17 25 52.66 21.9G 10VE253 F51 C~434g 2010 11 03.475325 01 42 46.419 +17 25 51.97 21.7G 10VE253 F51 C~434g 2011 01 25.235635 01 38 09.359 +16 42 51.59 21.8G 10VE253 F51 C~434g 2011 01 25.240419 01 38 09.374 +16 42 51.49 22.4G 10VE253 F51 C~434g 2011 01 25.245479 01 38 09.409 +16 42 51.49 22.4G 10VE253 F51 C~434g 2011 01 25.250257 01 38 09.426 +16 42 51.68 22.1G 10VE253 F51 C~434g 2011 11 14.288161 02 07 34.120 +20 15 53.31 21.4G 10VE253 F51 C~434g 2011 11 14.300049 02 07 34.022 +20 15 52.32 22.2G 10VE253 F51 C~434g 2011 11 30.301502 02 05 04.443 +20 01 30.96 21.7G 10VE253 F51 C~434g 2012 10 19.553557 02 39 41.926 +23 18 19.40 21.7G 10VE253 F51 C~434g 2012 10 24.530103 02 38 47.980 +23 15 20.61 22.4G 10VE253 F51 C~434g 2012 10 24.543823 02 38 47.824 +23 15 19.93 21.9G 10VE253 F51 C~434g 2012 11 03.499677 02 36 56.600 +23 08 24.50 22.3G 10VE253 F51 C~434g 2012 11 04.345814 02 36 47.104 +23 07 46.07 21.9G 10VE253 F51 C~434g 2012 11 04.357914 02 36 46.966 +23 07 45.41 22.2G 10VE253 F51 C~434g 2012 11 05.450310 02 36 34.626 +23 06 55.38 21.8G 10VE253 F51 C~434g 2012 11 05.462480 02 36 34.500 +23 06 54.74 22.2G 10VE253 F51 C~434g 2013 10 24.574773 03 07 08.421 +25 37 19.89 21.9G 10VE253 F51 C~434g 2013 10 24.587866 03 07 08.314 +25 37 19.35 20.8G 10VE253 F51 C~434g 2013 10 30.490708 03 06 03.550 +25 34 21.31 22.1G 10VE253 F51 C~434g 2013 10 30.505071 03 06 03.365 +25 34 20.80 22.0G 10VE253 F51 C~434g 2014 11 11.347839 03 32 34.216 +27 28 31.73 21.9G 10VE253 F51 C~434g 2014 11 22.482368 03 30 23.694 +27 21 57.51 21.7G 10VE253 F51 C~434g 2014 11 22.494739 03 30 23.560 +27 21 56.99 21.9G 10VE253 F51 C~434g 2014 11 22.507089 03 30 23.413 +27 21 56.50 22.1G 10VE253 F51 C~434g 2014 11 22.519458 03 30 23.278 +27 21 56.14 22.1G 10VE253 F51 C~434g 2014 12 09.441897 03 27 14.572 +27 09 58.56 21.6G 10VE253 F51 C~434g 2014 12 09.454256 03 27 14.446 +27 09 57.73 21.6G 10VE253 F51 C~434g 2014 12 09.466667 03 27 14.314 +27 09 57.10 21.7G 10VE253 F51 C~434g 2014 12 09.479041 03 27 14.176 +27 09 56.76 21.5G 10VE253 F51 C~434g 2014 12 18.200212 03 25 49.045 +27 03 21.36 21.0G 10VE253 F51 C~434g 2014 12 20.390728 03 25 29.470 +27 01 42.22 22.1G 10VE253 F51 C~434g 2014 12 20.402899 03 25 29.340 +27 01 41.78 22.6G 10VE253 F51 C~434g 2014 12 20.414997 03 25 29.231 +27 01 41.15 22.3G 10VE253 F51 C~434g 2014 12 20.427128 03 25 29.113 +27 01 40.47 22.3G 10VE253 F51 C~434g 2015 01 19.324119 03 22 41.466 +26 41 32.30 21.8G 10VE253 F51 C~434g 2015 01 19.336266 03 22 41.441 +26 41 31.76 22.2G 10VE253 F51 C~434h 2015 01 19.348449 03 22 41.419 +26 41 31.28 22.0G 10VE253 F51 C~434h 2015 01 19.360734 03 22 41.384 +26 41 31.00 22.3G 10VE253 F51 C~434h 2015 01 21.275549 03 22 37.927 +26 40 30.02 22.8G 10VE253 F51 C~434h 2015 01 21.288088 03 22 37.897 +26 40 29.70 22.3G 10VE253 F51 C~434h 2015 01 21.300519 03 22 37.879 +26 40 29.38 22.7G 10VE253 F51 C~434h 2015 01 21.313042 03 22 37.851 +26 40 28.91 22.3G 10VE253 F51 C~434h 2016 02 03.284007 03 49 54.998 +28 15 27.75 22.7G 10VE253 F51 C~434h 2016 02 03.295982 03 49 54.977 +28 15 26.75 23.1G 10VE253 F51 C~434h 2016 02 03.307954 03 49 54.975 +28 15 27.14 22.9G 10VE253 F51 C~434h 2016 12 22.422509 04 21 49.303 +29 58 12.78 22.2G 10VE253 F51 C~434h 2016 12 22.434604 04 21 49.183 +29 58 12.14 22.3G 10VE253 F51 C~434h 2016 12 22.446707 04 21 49.015 +29 58 12.00 22.5G 10VE253 F51 C~434h 2016 12 22.458835 04 21 48.891 +29 58 11.22 22.3G 10VE253 F51 C~434h 2017 01 29.303297 04 17 20.185 +29 35 31.83 21.9G 10VE253 F51 C~434h 2017 01 29.311330 04 17 20.172 +29 35 31.17 22.3G 10VE253 F51 C~434h 2017 01 29.313447 04 17 20.188 +29 35 31.51 22.9G 10VE253 F51 C~434h 2017 01 29.323508 04 17 20.140 +29 35 30.88 22.0G 10VE253 F51 C~434h 2021 02 15.218610 05 58 34.493 +31 04 35.24 23.0G 10VE253 G37 C~4Z2T 2021 02 15.271730 05 58 34.247 +31 04 33.99 10VE253 G37 C~4Z2T
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 0.17 0.00 -0.23
2 0.0000 0.00 -0.15 0.00 -0.15
3 0.8350 0.00 -0.07 0.00 0.21
4 0.8404 0.00 0.12 0.00 0.32
5 0.8404 0.00 0.15 0.00 -0.28
6 1.0485 0.00 0.11 0.00 -0.14
7 1.0485 0.00 -0.28 0.00 -0.18
8 1.0590 0.00 -0.09 0.00 -0.07
9 1.0590 0.00 0.00 0.00 -0.00
10 1.0591 0.00 -0.03 0.00 0.01
11 1.0591 0.00 -0.01 0.00 0.05
12 1.1217 0.00 0.42 0.00 0.09
13 1.1298 0.00 0.23 0.00 0.22
14 1.1298 0.00 -0.09 0.00 -0.22
15 1.1298 0.00 -0.43 0.00 0.14
16 1.1298 0.00 -0.17 0.00 -0.00
17 1.1331 0.00 -0.10 0.00 0.07
18 1.1331 0.00 0.06 0.00 0.01
19 1.1332 0.00 -0.09 0.00 0.03
20 1.3597 0.00 0.23 0.00 0.20
21 1.3598 0.00 0.04 0.00 0.02
22 1.3598 0.00 0.13 0.00 -0.05
23 1.3598 0.00 -0.03 0.00 0.07
24 2.1621 0.00 -0.44 0.00 0.07
25 2.1621 0.00 -0.05 0.00 -0.28
26 2.2059 0.00 -0.06 0.00 -0.06
27 3.0937 0.00 0.21 0.00 -0.10
28 3.1073 0.00 0.16 0.00 -0.01
29 3.1073 0.00 0.12 0.00 -0.16
30 3.1346 0.00 0.02 0.00 0.15
31 3.1369 0.00 0.01 0.00 0.11
32 3.1369 0.00 0.02 0.00 -0.00
33 3.1399 0.00 -0.23 0.00 0.15
34 3.1400 0.00 -0.02 0.00 0.07
35 4.1067 0.00 -0.36 0.00 0.21
36 4.1068 0.00 0.18 0.00 0.05
37 4.1229 0.00 0.21 0.00 0.18
38 4.1230 0.00 -0.10 0.00 0.15
39 5.1547 0.00 -0.05 0.00 0.13
40 5.1852 0.00 -0.06 0.00 -0.01
41 5.1852 0.00 0.14 0.00 -0.04
42 5.1853 0.00 0.14 0.00 -0.04
43 5.1853 0.00 0.31 0.00 0.09
44 5.2316 0.00 -0.22 0.00 0.10
45 5.2317 0.00 -0.15 0.00 -0.17
46 5.2317 0.00 -0.16 0.00 -0.23
47 5.2317 0.00 -0.27 0.00 -0.00
48 5.2556 0.00 -0.16 0.00 -0.27
49 5.2616 0.00 0.36 0.00 -0.10
50 5.2616 0.00 0.04 0.00 0.02
51 5.2617 0.00 0.03 0.00 -0.06
52 5.2617 0.00 -0.11 0.00 -0.18
53 5.3436 0.00 -0.01 0.00 0.07
54 5.3436 0.00 0.03 0.00 -0.06
55 5.3436 0.00 0.11 0.00 -0.14
56 5.3437 0.00 -0.00 0.00 -0.00
57 5.3489 0.00 0.08 0.00 -0.08
58 5.3489 0.00 -0.03 0.00 -0.00
59 5.3490 0.00 0.03 0.00 0.07
60 5.3490 0.00 -0.06 0.00 -0.00
61 6.3838 0.00 0.29 0.00 0.15
62 6.3839 0.00 0.01 0.00 -0.51
63 6.3839 0.00 0.02 0.00 0.21
64 7.2685 0.00 0.01 0.00 0.03
65 7.2686 0.00 0.16 0.00 -0.18
66 7.2686 0.00 -0.41 0.00 0.11
67 7.2686 0.00 -0.31 0.00 -0.23
68 7.3722 0.00 -0.17 0.00 0.32
69 7.3723 0.00 0.01 0.00 -0.08
70 7.3723 0.00 0.35 0.00 0.33
71 7.3723 0.00 0.09 0.00 0.04
72 11.4186 0.00 0.03 0.00 -0.01
73 11.4187 0.00 0.05 0.00 0.02
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.
10VE253 quality flag:3 Type: CENTAURR CENTAURR CENTAURR axisobj 32.153 32.153 32.153 ecceobj 0.487 0.487 0.487 incobj 7.888 7.888 7.888 qmin 16.352 16.353 16.327 qmax 47.824 47.823 47.825 amean 31.759 31.777 31.731 amin 31.434 31.422 31.302 amax 32.153 32.153 32.153 emean 0.479 0.479 0.479 emin 0.472 0.472 0.472 emax 0.487 0.487 0.487 imean 9.188 9.189 9.132 imin 8.900 8.900 8.900 imax 9.444 9.411 9.327 excite_mean 0.505 0.505 0.505 fracstop 0.003 0.004 0.002 cjmean 2.725 2.725 2.725 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 62.1 63.8 60.5 kozaiamp 8.6 10.3 7.3