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: 535029 # Created Fri Apr 19 01:08:46 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 83 observations of 83 # Arc: 12.05y # First observation: 2010/09/06 # Last observation: 2022/09/26 # Chi-squared of fit: 61.39 DOF: 160 RMS: 0.15 # Min/Max residuals: -0.43 0.66 # Exact a, adot, b, bdot, g, gdot: 1.650749E-05 3.031235E-02 -1.068794E-06 -2.486323E-03 2.828978E-02 6.883583E-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 -16.833695 61.703436 0.981282 -0.060885 -0.201163 2455446.134246 # Heliocentric elements and errors Epoch: 2455446.5000 = 2010/09/07 Mean Anomaly: 52.29541 +/- 0.000 Argument of Peri: 178.21709 +/- 0.000 Long of Asc Node: 167.35145 +/- 0.000 Inclination: 17.47459 +/- 0.000 Eccentricity: 0.21722532 +/- 0.0000 Semi-Major Axis: 39.39211016 +/- 0.0000 Time of Perihelion: 2442328.3278 +/- 0.0 Perihelion: 30.83514627 +/- 0.0000 Aphelion: 47.94907404 +/- 0.0000 Period (y) 247.2419 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 17.00572625 +/- 0.0000 Ecliptic Y 29.50953433 +/- 0.0000 Ecliptic Z -10.23675738 +/- 0.0000 Ecliptic XDOT -0.00231326 +/- 0.0000 Ecliptic YDOT 0.00189705 +/- 0.0000 Ecliptic ZDOT -0.00042326 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 35.56388633 +/- 0.0000 Geocenter to KBO 35.34834652 +/- 0.0000 # Hcoef: 6.62
The following table shows the complete astrometric record for 535029. 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 (535029) followed by the observatory code and reference code for the source of the astrometry.
2010 09 06.63348 04 11 47.138 +03 59 15.01 22.0G 535029 F51 C~2rYG 2010 09 15.62023 04 11 43.015 +03 54 37.06 21.9G 535029 F51 C~2rYG 2010 11 11.51292 04 08 21.569 +03 25 42.37 21.7G 535029 F51 C~2rYG 2010 11 18.34270 04 07 44.075 +03 23 11.76 21.7G 535029 F51 C~2rYG 2010 11 18.35336 04 07 44.038 +03 23 11.59 21.8G 535029 F51 C~2rYG 2011 10 18.61207 04 17 19.650 +03 48 30.00 22.6G 535029 F51 C~2rYG 2011 10 20.60945 04 17 11.641 +03 47 29.08 22.3G 535029 F51 C~2rYG 2011 10 23.44164 04 16 59.774 +03 46 04.27 22.1w 535029 F51 C~1vXu 2011 10 23.45653 04 16 59.706 +03 46 03.73 22.1w 535029 F51 C~1vXu 2011 10 23.47140 04 16 59.640 +03 46 03.50 21.9w 535029 F51 C~1vXu 2011 10 23.48635 04 16 59.578 +03 46 02.73 22.0w 535029 F51 C~1vXu 2011 10 25.57538 04 16 50.462 +03 45 01.25 22.5G 535029 F51 C~2rYG 2012 10 20.54113 04 24 05.798 +03 58 20.02 22.4G 535029 F51 C~2rYG 2013 01 25.30401 04 16 30.988 +03 45 50.08 22.2G 535029 F51 C~2rYG 2013 01 27.34305 04 16 26.512 +03 46 30.72 22.6G 535029 F51 C~2rYG 2013 08 24.62108 04 32 00.522 +04 37 23.80 22.1G 535029 F51 C~2rYG 2013 11 06.45925 04 29 43.301 +04 01 36.52 21.8G 535029 F51 C~2rYG 2014 01 21.24479 04 23 32.810 +03 55 30.53 22.3w 535029 F51 C~1vXu 2014 01 21.25766 04 23 32.766 +03 55 30.79 22.4w 535029 F51 C~1vXu 2014 01 21.27064 04 23 32.728 +03 55 31.05 22.4w 535029 F51 C~1vXu 2014 01 21.28370 04 23 32.687 +03 55 31.20 22.2w 535029 F51 C~1vXu 2014 09 18.60507 04 38 56.794 +04 35 51.59 22.4G 535029 F51 C~2rYG 2014 10 26.57092 04 37 22.278 +04 16 53.51 22.6G 535029 F51 C~2rYG 2014 10 26.59575 04 37 22.165 +04 16 53.03 22.2G 535029 F51 C~2rYG 2014 11 21.46933 04 35 14.994 +04 06 56.20 21.7G 535029 F51 C~2rYG 2014 11 21.48151 04 35 14.918 +04 06 56.13 22.0G 535029 F51 C~2rYG 2014 11 21.49362 04 35 14.853 +04 06 55.72 22.1G 535029 F51 C~2rYG 2014 11 21.50574 04 35 14.784 +04 06 55.51 22.2G 535029 F51 C~2rYG 2014 11 23.46046 04 35 04.095 +04 06 21.62 21.9w 535029 F51 C~1vXu 2014 11 23.47262 04 35 04.034 +04 06 21.61 22.1w 535029 F51 C~1vXu 2014 11 23.48476 04 35 03.947 +04 06 21.36 22.0w 535029 F51 C~1vXu 2014 11 23.49694 04 35 03.875 +04 06 21.34 22.0w 535029 F51 C~1vXu 2015 01 09.25981 04 31 02.598 +04 03 24.48 22.2w 535029 F51 C~1vXu 2015 01 09.27288 04 31 02.547 +04 03 24.72 22.1w 535029 F51 C~1vXu 2015 01 09.28597 04 31 02.480 +04 03 24.90 22.4w 535029 F51 C~1vXu 2015 01 09.29910 04 31 02.427 +04 03 24.97 22.0w 535029 F51 C~1vXu 2015 01 15.22470 04 30 39.716 +04 04 33.25 22.3w 535029 F51 C~1vXu 2015 01 15.23625 04 30 39.656 +04 04 33.44 22.4w 535029 F51 C~1vXu 2015 01 15.24773 04 30 39.624 +04 04 33.52 22.2w 535029 F51 C~1vXu 2015 01 15.25924 04 30 39.574 +04 04 33.76 22.3w 535029 F51 C~1vXu 2015 01 19.22672 04 30 26.022 +04 05 30.36 22.1w 535029 F51 C~1vXu 2015 01 19.25088 04 30 25.943 +04 05 30.83 22.2w 535029 F51 C~1vXu 2015 01 19.26298 04 30 25.901 +04 05 31.00 22.2w 535029 F51 C~1vXu 2015 10 21.53993 04 44 24.417 +04 29 20.06 22.1G 535029 F51 C~2rYG 2015 10 21.55186 04 44 24.362 +04 29 20.10 22.2G 535029 F51 C~2rYG 2015 10 21.56374 04 44 24.337 +04 29 20.06 21.7G 535029 F51 C~2rYG 2015 10 21.57558 04 44 24.288 +04 29 19.79 21.7G 535029 F51 C~2rYG 2015 10 22.41741 04 44 21.188 +04 28 55.24 21.9G 535029 F51 C~2rYG 2015 10 22.44190 04 44 21.101 +04 28 54.76 22.4G 535029 F51 C~2rYG 2015 10 22.45421 04 44 21.088 +04 28 54.22 21.6G 535029 F51 C~2rYG 2015 11 02.55733 04 43 35.233 +04 23 58.78 22.0G 535029 F51 C~2rYG 2015 11 02.56924 04 43 35.208 +04 23 58.58 22.8G 535029 F51 C~2rYG 2015 11 02.58112 04 43 35.151 +04 23 58.17 22.1G 535029 F51 C~2rYG 2015 11 02.59299 04 43 35.081 +04 23 57.71 23.0G 535029 F51 C~2rYG 2015 11 18.44227 04 42 16.678 +04 18 06.60 22.0G 535029 F51 C~2rYG 2015 11 18.45433 04 42 16.616 +04 18 06.40 22.4G 535029 F51 C~2rYG 2015 11 18.48314 04 42 16.462 +04 18 05.39 22.3G 535029 F51 C~2rYG 2015 12 03.35750 04 40 55.101 +04 14 17.45 21.9G 535029 F51 C~2rYG 2015 12 03.35900 04 40 55.081 +04 14 17.43 22.4G 535029 F51 C~2rYG 2015 12 03.36951 04 40 55.021 +04 14 17.47 22.0G 535029 F51 C~2rYG 2015 12 03.37101 04 40 55.012 +04 14 17.27 21.9G 535029 F51 C~2rYG 2015 12 03.38155 04 40 54.966 +04 14 17.17 22.0G 535029 F51 C~2rYG 2015 12 03.38304 04 40 54.952 +04 14 17.17 22.2G 535029 F51 C~2rYG 2015 12 03.39366 04 40 54.882 +04 14 17.06 22.0G 535029 F51 C~2rYG 2015 12 03.39514 04 40 54.883 +04 14 16.98 22.1G 535029 F51 C~2rYG 2016 01 14.36543 04 37 25.909 +04 14 33.80 22.4G 535029 F51 C~2rYG 2016 11 24.45347 04 48 19.343 +04 25 58.20 21.7G 535029 F51 C~2rYG 2017 01 24.25551 04 43 26.286 +04 27 06.35 22.3G 535029 F51 C~2rYG 2017 02 14.25460 04 42 45.060 +04 34 53.24 22.3G 535029 F51 C~2rYG 2017 02 14.26586 04 42 45.048 +04 34 53.59 22.4G 535029 F51 C~2rYG 2017 02 14.27716 04 42 45.036 +04 34 54.05 21.9G 535029 F51 C~2rYG 2017 02 14.28852 04 42 45.028 +04 34 54.21 22.4G 535029 F51 C~2rYG 2017 12 23.31395 04 52 17.196 +04 31 44.94 22.6G 535029 F51 C~2rYG 2017 12 23.32531 04 52 17.128 +04 31 44.98 22.5G 535029 F51 C~2rYG 2017 12 23.33677 04 52 17.064 +04 31 45.02 23.0G 535029 F51 C~2rYG 2017 12 23.34829 04 52 16.998 +04 31 45.10 22.8G 535029 F51 C~2rYG 2018 01 06.35887 04 51 08.053 +04 32 43.29 22.1G 535029 F51 C~2rYG 2018 01 06.37097 04 51 08.003 +04 32 43.16 22.6G 535029 F51 C~2rYG 2018 01 06.38313 04 51 07.946 +04 32 43.40 23.3G 535029 F51 C~2rYG 2018 01 06.39520 04 51 07.886 +04 32 43.71 21.8G 535029 F51 C~2rYG 2022 09 26.605363 05 29 31.091 +05 40 26.25 22.2w 535029 F52 C~5t9P 2022 09 26.618235 05 29 31.089 +05 40 25.52 22.5w 535029 F52 C~5t9P 2022 09 26.624700 05 29 31.080 +05 40 25.67 22.5w 535029 F52 C~5t9P
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 0.10 0.00 -0.05
2 0.0246 0.00 0.13 0.00 -0.30
3 0.1804 0.00 -0.07 0.00 0.03
4 0.1991 0.00 -0.18 0.00 -0.15
5 0.1991 0.00 0.17 0.00 -0.10
6 1.1142 0.00 0.04 0.00 -0.11
7 1.1197 0.00 -0.01 0.00 -0.06
8 1.1275 0.00 -0.22 0.00 0.17
9 1.1275 0.00 -0.26 0.00 0.07
10 1.1276 0.00 -0.27 0.00 0.28
11 1.1276 0.00 -0.22 0.00 -0.04
12 1.1333 0.00 0.15 0.00 -0.03
13 2.1216 0.00 0.15 0.00 0.01
14 2.3865 0.00 0.13 0.00 -0.03
15 2.3921 0.00 0.28 0.00 0.21
16 2.9651 0.00 0.05 0.00 -0.04
17 3.1672 0.00 0.20 0.00 -0.11
18 3.3747 0.00 0.19 0.00 -0.17
19 3.3747 0.00 0.11 0.00 -0.13
20 3.3748 0.00 0.12 0.00 -0.08
21 3.3748 0.00 0.09 0.00 -0.15
22 4.0328 0.00 0.08 0.00 -0.18
23 4.1367 0.00 0.23 0.00 -0.05
24 4.1368 0.00 0.12 0.00 0.15
25 4.2076 0.00 0.09 0.00 0.05
26 4.2077 0.00 -0.03 0.00 0.19
27 4.2077 0.00 0.00 0.00 0.00
28 4.2077 0.00 -0.03 0.00 0.01
29 4.2131 0.00 0.10 0.00 -0.14
30 4.2131 0.00 0.21 0.00 0.05
31 4.2131 0.00 -0.08 0.00 0.00
32 4.2132 0.00 -0.14 0.00 0.19
33 4.3412 0.00 -0.07 0.00 -0.08
34 4.3412 0.00 -0.01 0.00 0.03
35 4.3413 0.00 -0.20 0.00 0.08
36 4.3413 0.00 -0.18 0.00 0.02
37 4.3575 0.00 0.01 0.00 0.03
38 4.3576 0.00 -0.25 0.00 0.07
39 4.3576 0.00 -0.10 0.00 -0.00
40 4.3576 0.00 -0.21 0.00 0.09
41 4.3685 0.00 -0.07 0.00 0.09
42 4.3686 0.00 -0.04 0.00 0.18
43 4.3686 0.00 -0.07 0.00 0.17
44 5.1223 0.00 -0.03 0.00 -0.08
45 5.1223 0.00 -0.19 0.00 0.30
46 5.1223 0.00 0.10 0.00 0.59
47 5.1224 0.00 0.03 0.00 0.66
48 5.1247 0.00 -0.32 0.00 -0.23
49 5.1247 0.00 -0.24 0.00 -0.02
50 5.1248 0.00 0.27 0.00 -0.22
51 5.1552 0.00 -0.37 0.00 -0.04
52 5.1552 0.00 0.08 0.00 0.06
53 5.1552 0.00 0.05 0.00 -0.06
54 5.1553 0.00 -0.19 0.00 -0.22
55 5.1987 0.00 0.03 0.00 0.00
56 5.1987 0.00 0.08 0.00 0.03
57 5.1988 0.00 0.10 0.00 -0.43
58 5.2395 0.00 0.16 0.00 -0.07
59 5.2395 0.00 -0.01 0.00 -0.07
60 5.2395 0.00 -0.02 0.00 0.09
61 5.2395 0.00 -0.03 0.00 -0.10
62 5.2396 0.00 0.17 0.00 -0.07
63 5.2396 0.00 0.09 0.00 -0.06
64 5.2396 0.00 -0.06 0.00 -0.04
65 5.2396 0.00 0.08 0.00 -0.11
66 5.3545 0.00 -0.12 0.00 0.13
67 6.2172 0.00 0.08 0.00 -0.07
68 6.3836 0.00 0.03 0.00 0.14
69 6.4411 0.00 -0.05 0.00 -0.07
70 6.4412 0.00 -0.07 0.00 -0.02
71 6.4412 0.00 -0.09 0.00 0.15
72 6.4412 0.00 -0.05 0.00 0.01
73 7.2955 0.00 0.14 0.00 -0.10
74 7.2955 0.00 0.03 0.00 -0.06
75 7.2956 0.00 -0.01 0.00 -0.03
76 7.2956 0.00 -0.08 0.00 0.05
77 7.3340 0.00 0.03 0.00 0.09
78 7.3340 0.00 0.13 0.00 -0.14
79 7.3340 0.00 0.12 0.00 0.01
80 7.3340 0.00 0.06 0.00 0.22
81 12.0547 0.00 0.02 0.00 0.05
82 12.0547 0.00 0.05 0.00 -0.33
83 12.0547 0.00 -0.06 0.00 -0.01
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.
535029 quality flag:3 Type: 3:2E 3:2E 3:2E axisobj 39.603 39.603 39.602 ecceobj 0.220 0.220 0.220 incobj 17.463 17.463 17.463 qmin 28.119 28.165 28.146 qmax 51.466 51.475 51.492 amean 39.455 39.455 39.455 amin 38.956 38.929 38.964 amax 40.017 40.039 40.044 emean 0.236 0.239 0.237 emin 0.181 0.181 0.181 emax 0.287 0.287 0.287 imean 16.041 15.937 16.024 imin 14.040 14.086 14.053 imax 18.000 18.001 18.000 excite_mean 0.365 0.365 0.365 fracstop 1.000 1.000 1.000 cjmean 2.900 2.900 2.900 libcent 0 179.6 180.0 179.6 libamp 0 110.4 110.2 110.3 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 97.1 101.1 97.6 kozaiamp 80.3 85.0 80.4