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: 523793 # Created Thu Apr 18 01:08:31 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 83 observations of 83 # Arc: 10.12y # First observation: 2013/08/24 # Last observation: 2023/10/09 # Chi-squared of fit: 57.02 DOF: 160 RMS: 0.15 # Min/Max residuals: -0.77 0.44 # Exact a, adot, b, bdot, g, gdot: 1.293994E-05 2.176573E-02 -6.372676E-06 -1.107834E-02 2.504626E-02 -2.128980E-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 -14.990244 -36.145190 -0.127674 -0.259714 -0.970078 2456528.920138 # Heliocentric elements and errors Epoch: 2456528.5000 = 2013/08/24 Mean Anomaly: 268.74161 +/- 0.000 Argument of Peri: 311.32263 +/- 0.000 Long of Asc Node: 117.63410 +/- 0.000 Inclination: 30.40357 +/- 0.000 Eccentricity: 0.08913125 +/- 0.0000 Semi-Major Axis: 40.49750955 +/- 0.0000 Time of Perihelion: 2480390.7409 +/- 0.0 Perihelion: 36.88791583 +/- 0.0000 Aphelion: 44.10710327 +/- 0.0000 Period (y) 257.7215 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 32.03047900 +/- 0.0000 Ecliptic Y -23.23464970 +/- 0.0000 Ecliptic Z -10.32728305 +/- 0.0000 Ecliptic XDOT 0.00096269 +/- 0.0000 Ecliptic YDOT 0.00223763 +/- 0.0000 Ecliptic ZDOT -0.00110945 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 40.89569371 +/- 0.0000 Geocenter to KBO 39.92620230 +/- 0.0000 # Hcoef: 5.90
The following table shows the complete astrometric record for 523793. 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 (523793) followed by the observatory code and reference code for the source of the astrometry.
2013 08 24.41936 22 06 50.076 -27 38 32.00 22.2G 523793 F51 C~2kRp 2013 09 01.40804 22 06 09.072 -27 42 16.63 22.0G 523793 F51 C~2kRp 2014 07 02.54257 22 16 57.261 -27 13 06.87 21.9w 523793 F51 C~1vYk 2014 07 02.55248 22 16 57.221 -27 13 06.91 22.1w 523793 F51 C~1vYk 2014 07 02.56237 22 16 57.210 -27 13 07.57 22.0w 523793 F51 C~1vYk 2014 07 02.57228 22 16 57.176 -27 13 08.06 21.7w 523793 F51 C~1vYk 2014 07 04.53433 22 16 51.670 -27 14 25.15 21.9G 523793 F51 C~2kRp 2014 07 04.54418 22 16 51.642 -27 14 25.53 22.5G 523793 F51 C~2kRp 2014 07 04.55404 22 16 51.617 -27 14 25.73 22.2G 523793 F51 C~2kRp 2014 07 04.56389 22 16 51.590 -27 14 26.17 21.7G 523793 F51 C~2kRp 2014 07 31.50261 22 15 08.179 -27 32 15.37 22.1w 523793 F51 C~1vYk 2014 07 31.51260 22 15 08.140 -27 32 15.74 22.1w 523793 F51 C~1vYk 2014 07 31.52256 22 15 08.105 -27 32 15.98 21.8w 523793 F51 C~1vYk 2014 07 31.53251 22 15 08.055 -27 32 16.58 22.3w 523793 F51 C~1vYk 2014 09 02.40117 22 12 22.946 -27 50 39.78 22.0G 523793 F51 C~2kRp 2014 09 02.41173 22 12 22.891 -27 50 40.05 21.8G 523793 F51 C~2kRp 2014 09 02.42227 22 12 22.825 -27 50 40.47 22.1G 523793 F51 C~2kRp 2014 09 02.43284 22 12 22.770 -27 50 40.61 21.9G 523793 F51 C~2kRp 2014 09 16.36107 22 11 14.236 -27 55 57.28 21.7G 523793 F51 C~2kRp 2014 09 20.40750 22 10 55.595 -27 57 08.78 21.7G 523793 F51 C~2kRp 2014 09 21.04129 22 10 52.78 -27 57 17.9 22.3V 523793 W84 C~2gaG 2014 09 21.12911 22 10 52.38 -27 57 19.3 523793 W84 C~2gaG 2014 09 22.04253 22 10 48.33 -27 57 33.4 523793 W84 C~2gaG 2015 07 26.50122 22 21 50.581 -27 35 16.04 21.9w 523793 F51 C~1vYk 2015 07 26.51144 22 21 50.542 -27 35 16.56 21.9w 523793 F51 C~1vYk 2015 07 26.52179 22 21 50.500 -27 35 16.97 22.1w 523793 F51 C~1vYk 2015 07 26.53208 22 21 50.453 -27 35 17.30 22.1w 523793 F51 C~1vYk 2015 07 27.54616 22 21 46.093 -27 35 58.14 22.1w 523793 F51 C~1vYk 2015 07 27.54631 22 21 46.104 -27 35 58.19 22.1G 523793 F51 C~2kRp 2015 07 27.55678 22 21 46.037 -27 35 58.48 22.0w 523793 F51 C~1vYk 2015 07 27.55685 22 21 46.043 -27 35 58.55 22.2G 523793 F51 C~2kRp 2015 07 27.56740 22 21 45.994 -27 35 58.88 22.0w 523793 F51 C~1vYk 2015 07 27.57793 22 21 45.942 -27 35 59.49 22.3w 523793 F51 C~1vYk 2015 08 07.53765 22 20 55.649 -27 43 09.33 21.9G 523793 F51 C~2kRp 2016 07 16.56337 22 28 47.397 -27 34 15.72 21.8G 523793 F51 C~2kRp 2016 08 06.49122 22 27 19.022 -27 48 29.46 21.9G 523793 F51 C~2kRp 2016 08 06.50095 22 27 18.982 -27 48 29.68 22.3G 523793 F51 C~2kRp 2016 08 06.52025 22 27 18.893 -27 48 30.37 21.9G 523793 F51 C~2kRp 2016 08 11.45564 22 26 54.996 -27 51 39.98 21.9G 523793 F51 C~2kRp 2016 08 11.46708 22 26 54.930 -27 51 40.36 22.0G 523793 F51 C~2kRp 2016 08 11.47853 22 26 54.887 -27 51 40.86 22.0G 523793 F51 C~2kRp 2016 08 11.48997 22 26 54.820 -27 51 41.19 21.9G 523793 F51 C~2kRp 2016 08 30.41262 22 25 18.322 -28 02 24.68 21.8G 523793 F51 C~2kRp 2016 08 30.42227 22 25 18.257 -28 02 24.95 22.1G 523793 F51 C~2kRp 2016 08 30.43193 22 25 18.210 -28 02 25.37 22.4G 523793 F51 C~2kRp 2016 08 30.44158 22 25 18.170 -28 02 25.74 21.8G 523793 F51 C~2kRp 2016 09 07.38314 22 24 37.428 -28 06 05.10 21.7G 523793 F51 C~2kRp 2016 09 07.39348 22 24 37.384 -28 06 05.24 21.9G 523793 F51 C~2kRp 2016 09 07.40380 22 24 37.340 -28 06 05.48 21.8G 523793 F51 C~2kRp 2016 09 07.41413 22 24 37.277 -28 06 05.69 21.7G 523793 F51 C~2kRp 2016 10 06.33491 22 22 26.737 -28 13 53.06 22.0G 523793 F51 C~2kRp 2016 10 19.29783 22 21 45.002 -28 14 14.60 22.3G 523793 F51 C~2kRp 2016 10 26.27719 22 21 28.437 -28 13 37.42 22.4G 523793 F51 C~2kRp 2017 06 24.56739 22 36 06.551 -27 23 09.26 21.6G 523793 F51 C~2kRp 2017 08 14.42929 22 33 06.221 -27 57 52.68 22.0G 523793 F51 C~2kRp 2017 08 14.43948 22 33 06.173 -27 57 53.03 21.7G 523793 F51 C~2kRp 2017 08 14.44965 22 33 06.118 -27 57 53.42 22.1G 523793 F51 C~2kRp 2017 08 14.45980 22 33 06.069 -27 57 53.82 22.4G 523793 F51 C~2kRp 2017 09 15.36836 22 30 23.502 -28 14 04.86 21.9G 523793 F51 C~2kRp 2017 09 15.37738 22 30 23.457 -28 14 05.15 21.7G 523793 F51 C~2kRp 2017 09 15.38640 22 30 23.404 -28 14 05.17 22.1G 523793 F51 C~2kRp 2017 09 15.39541 22 30 23.362 -28 14 05.34 22.1G 523793 F51 C~2kRp 2020 06 28.53681 22 55 10.932 -27 30 55.04 22.3w 523793 F51 C~3ywh 2020 06 28.54739 22 55 10.915 -27 30 55.54 22.0w 523793 F51 C~3ywh 2020 06 28.55795 22 55 10.875 -27 30 55.99 22.1w 523793 F51 C~3ywh 2020 06 28.56851 22 55 10.875 -27 30 56.36 22.0w 523793 F51 C~3ywh 2020 07 25.51193 22 53 59.404 -27 50 28.65 21.9w 523793 F51 C~430v 2020 07 25.52148 22 53 59.374 -27 50 29.05 21.8w 523793 F51 C~430v 2020 07 25.53102 22 53 59.333 -27 50 29.31 21.9w 523793 F51 C~430v 2021 09 08.391604 22 57 02.913 -28 19 29.22 21.7w 523793 F52 C~54uq 2021 09 08.402578 22 57 02.868 -28 19 29.56 21.9w 523793 F52 C~54uq 2021 09 08.413528 22 57 02.814 -28 19 29.78 21.7w 523793 F52 C~54uq 2021 09 08.424512 22 57 02.719 -28 19 29.91 21.6w 523793 F52 C~54uq 2023 08 19.450132 23 12 00.384 -28 04 02.14 21.6w 523793 F52 C~78vv 2023 08 19.460264 23 12 00.324 -28 04 02.45 21.7w 523793 F52 C~78vv 2023 08 19.470414 23 12 00.277 -28 04 02.68 22.0w 523793 F52 C~78vv 2023 09 11.414310 23 10 04.306 -28 18 00.78 21.8w 523793 F51 C~7AG6 2023 09 11.424381 23 10 04.248 -28 18 01.17 21.8w 523793 F51 C~7AG6 2023 09 11.434443 23 10 04.194 -28 18 01.66 21.7w 523793 F51 C~7AG6 2023 09 11.444536 23 10 04.133 -28 18 01.96 22.1w 523793 F51 C~7AG6 2023 10 09.305208 23 07 47.773 -28 27 28.24 22.2w 523793 F51 C~7MBj 2023 10 09.328322 23 07 47.670 -28 27 28.36 21.8w 523793 F51 C~7MBj 2023 10 09.347375 23 07 47.600 -28 27 28.55 22.0w 523793 F51 C~7MBj
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 0.23 0.00 -0.06
2 0.0219 0.00 -0.25 0.00 -0.10
3 0.8545 0.00 -0.06 0.00 0.09
4 0.8546 0.00 -0.24 0.00 0.44
5 0.8546 0.00 0.02 0.00 0.16
6 0.8546 0.00 -0.07 0.00 0.06
7 0.8600 0.00 0.07 0.00 -0.19
8 0.8600 0.00 0.09 0.00 -0.18
9 0.8601 0.00 0.16 0.00 0.00
10 0.8601 0.00 0.20 0.00 -0.05
11 0.9338 0.00 -0.19 0.00 0.04
12 0.9339 0.00 -0.07 0.00 0.06
13 0.9339 0.00 0.11 0.00 0.20
14 0.9339 0.00 0.06 0.00 -0.02
15 1.0239 0.00 0.20 0.00 -0.00
16 1.0239 0.00 0.20 0.00 0.01
17 1.0240 0.00 0.03 0.00 -0.13
18 1.0240 0.00 0.03 0.00 0.01
19 1.0621 0.00 0.12 0.00 0.23
20 1.0732 0.00 -0.19 0.00 -0.77
21 1.0749 0.00 0.10 0.00 0.04
22 1.0752 0.00 0.10 0.00 0.03
23 1.0777 0.00 0.17 0.00 -0.02
24 1.9195 0.00 -0.27 0.00 0.09
25 1.9195 0.00 -0.19 0.00 -0.02
26 1.9195 0.00 -0.14 0.00 -0.01
27 1.9195 0.00 -0.17 0.00 0.07
28 1.9223 0.00 -0.11 0.00 0.04
29 1.9223 0.00 0.07 0.00 -0.01
30 1.9223 0.00 -0.24 0.00 0.12
31 1.9223 0.00 -0.15 0.00 0.05
32 1.9224 0.00 -0.18 0.00 0.15
33 1.9224 0.00 -0.26 0.00 -0.04
34 1.9524 0.00 0.10 0.00 0.01
35 2.8943 0.00 0.26 0.00 0.16
36 2.9516 0.00 -0.03 0.00 0.01
37 2.9516 0.00 0.07 0.00 0.17
38 2.9517 0.00 0.14 0.00 0.23
39 2.9652 0.00 0.04 0.00 -0.07
40 2.9652 0.00 -0.09 0.00 -0.02
41 2.9653 0.00 0.13 0.00 -0.09
42 2.9653 0.00 -0.01 0.00 0.01
43 3.0171 0.00 0.16 0.00 0.04
44 3.0171 0.00 -0.06 0.00 0.06
45 3.0171 0.00 0.00 0.00 -0.07
46 3.0172 0.00 0.16 0.00 -0.16
47 3.0389 0.00 -0.08 0.00 -0.13
48 3.0389 0.00 0.06 0.00 -0.01
49 3.0390 0.00 0.20 0.00 0.01
50 3.0390 0.00 0.06 0.00 0.07
51 3.1182 0.00 0.18 0.00 0.14
52 3.1537 0.00 0.01 0.00 0.18
53 3.1728 0.00 -0.13 0.00 -0.26
54 3.8334 0.00 0.26 0.00 -0.41
55 3.9726 0.00 0.02 0.00 -0.05
56 3.9727 0.00 0.07 0.00 -0.02
57 3.9727 0.00 0.01 0.00 -0.02
58 3.9727 0.00 0.05 0.00 -0.04
59 4.0601 0.00 0.01 0.00 -0.08
60 4.0601 0.00 0.01 0.00 -0.17
61 4.0601 0.00 -0.10 0.00 0.00
62 4.0602 0.00 -0.06 0.00 0.03
63 6.8449 0.00 0.11 0.00 0.04
64 6.8450 0.00 0.10 0.00 -0.02
65 6.8450 0.00 -0.25 0.00 -0.03
66 6.8450 0.00 -0.01 0.00 0.03
67 6.9188 0.00 -0.06 0.00 0.08
68 6.9188 0.00 0.04 0.00 0.11
69 6.9189 0.00 -0.03 0.00 0.27
70 8.0410 0.00 -0.11 0.00 -0.12
71 8.0410 0.00 0.08 0.00 -0.13
72 8.0411 0.00 0.14 0.00 -0.02
73 8.0411 0.00 -0.41 0.00 0.18
74 9.9850 0.00 0.02 0.00 -0.11
75 9.9851 0.00 -0.15 0.00 0.00
76 9.9851 0.00 -0.11 0.00 0.20
77 10.0479 0.00 0.19 0.00 0.14
78 10.0479 0.00 0.12 0.00 0.06
79 10.0480 0.00 0.11 0.00 -0.13
80 10.0480 0.00 -0.00 0.00 -0.12
81 10.1243 0.00 -0.13 0.00 -0.12
82 10.1243 0.00 -0.13 0.00 -0.02
83 10.1244 0.00 0.10 0.00 -0.03
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.
523793 quality flag:3 Type: SCATEXTD SCATEXTD SCATEXTD axisobj 40.636 40.636 40.637 ecceobj 0.089 0.089 0.089 incobj 30.365 30.365 30.365 qmin 36.326 36.360 36.360 qmax 45.042 45.029 45.056 amean 40.597 40.596 40.596 amin 40.277 40.280 40.276 amax 40.925 40.929 40.932 emean 0.087 0.087 0.087 emin 0.074 0.074 0.074 emax 0.101 0.101 0.101 imean 28.809 28.809 28.809 imin 28.416 28.417 28.414 imax 29.198 29.193 29.193 excite_mean 0.490 0.490 0.490 fracstop 1.000 1.000 1.000 cjmean 2.769 2.769 2.769 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 177.3 177.2 177.2 kozaiamp 180.0 180.0 180.0