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: 531040 # Created Sat Apr 27 01:08:36 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 75 observations of 75 # Arc: 16.98y # First observation: 2005/03/10 # Last observation: 2022/03/02 # Chi-squared of fit: 143.68 DOF: 144 RMS: 0.24 # Min/Max residuals: -1.27 0.64 # Exact a, adot, b, bdot, g, gdot: 1.101498E-05 2.144671E-02 5.351885E-06 6.009124E-03 2.341421E-02 -1.087374E-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 -6.658623 127.692743 -0.660049 -0.085306 -0.731582 2453439.668046 # Heliocentric elements and errors Epoch: 2453440.5000 = 2005/03/11 Mean Anomaly: 274.51264 +/- 0.000 Argument of Peri: 66.61156 +/- 0.000 Long of Asc Node: 150.63247 +/- 0.000 Inclination: 16.98688 +/- 0.000 Eccentricity: 0.03565043 +/- 0.0000 Semi-Major Axis: 43.51513622 +/- 0.0000 Time of Perihelion: 2478338.1510 +/- 0.0 Perihelion: 41.96380289 +/- 0.0000 Aphelion: 45.06646955 +/- 0.0000 Period (y) 287.0574 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -26.91468782 +/- 0.0000 Ecliptic Y 33.74658741 +/- 0.0000 Ecliptic Z -4.95203291 +/- 0.0000 Ecliptic XDOT -0.00195693 +/- 0.0000 Ecliptic YDOT -0.00157594 +/- 0.0000 Ecliptic ZDOT 0.00071272 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 43.44832793 +/- 0.0000 Geocenter to KBO 42.70918665 +/- 0.0000 # Hcoef: 6.28
The following table shows the complete astrometric record for 531040. 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 (531040) followed by the observatory code and reference code for the source of the astrometry.
2005 03 10.167303 08 33 27.22 +11 54 10.3 531040 645 C~2VVI 2005 03 10.168132 08 33 27.21 +11 54 10.3 531040 645 C~2VVI 2005 12 06.386505 08 45 01.32 +11 26 53.1 531040 645 C~2VVI 2005 12 06.387334 08 45 01.32 +11 26 53.1 531040 645 C~2VVI 2005 12 06.389822 08 45 01.31 +11 26 53.1 531040 645 C~2VVI 2011 02 02.49885 09 07 31.022 +11 42 55.43 23.3w 531040 F51 C~1w3p 2011 02 02.51400 09 07 31.002 +11 42 56.05 21.7G 531040 F51 C~2rXr 2011 02 02.52986 09 07 30.909 +11 42 56.64 22.6G 531040 F51 C~2rXr 2011 02 02.54513 09 07 30.837 +11 42 57.09 22.7G 531040 F51 C~2rXr 2011 02 03.36760 09 07 27.008 +11 43 16.85 22.1G 531040 F51 C~2rXr 2011 02 03.38304 09 07 26.924 +11 43 17.58 22.4G 531040 F51 C~2rXr 2011 02 03.49389 09 07 26.386 +11 43 19.81 23.2w 531040 F51 C~1w3p 2012 02 03.54852 09 12 44.944 +11 42 25.44 22.3i 531040 F51 C~1w3p 2012 02 03.58203 09 12 44.816 +11 42 26.27 22.7r 531040 F51 C~1w3p 2012 02 22.42769 09 11 18.265 +11 50 25.81 23.0w 531040 F51 C~1w3p 2012 02 22.47810 09 11 18.044 +11 50 27.12 22.6G 531040 F51 C~2rXr 2013 02 03.34659 09 18 00.927 +11 41 26.10 22.5w 531040 F51 C~1w3p 2013 02 03.36121 09 18 00.861 +11 41 26.45 22.3w 531040 F51 C~1w3p 2013 02 03.39055 09 18 00.740 +11 41 27.00 22.6w 531040 F51 C~1w3p 2013 03 03.26444 09 15 55.630 +11 53 24.25 22.4w 531040 F51 C~1w3p 2013 03 03.27877 09 15 55.574 +11 53 24.69 22.6w 531040 F51 C~1w3p 2013 03 03.29314 09 15 55.505 +11 53 24.86 22.6w 531040 F51 C~1w3p 2013 03 03.30748 09 15 55.449 +11 53 25.42 22.9w 531040 F51 C~1w3p 2013 11 05.61658 09 26 47.154 +11 23 07.41 22.4w 531040 F51 C~1w3p 2014 01 05.45176 09 25 24.953 +11 28 52.05 22.1w 531040 F51 C~1w3p 2014 01 05.46693 09 25 24.898 +11 28 53.18 22.0w 531040 F51 C~1w3p 2014 01 05.48210 09 25 24.829 +11 28 53.17 22.4w 531040 F51 C~1w3p 2014 01 25.39372 09 24 02.315 +11 36 00.43 22.4w 531040 F51 C~1w3p 2014 01 25.40528 09 24 02.268 +11 36 00.88 22.4w 531040 F51 C~1w3p 2014 01 25.41679 09 24 02.237 +11 36 01.05 22.5w 531040 F51 C~1w3p 2014 02 20.35932 09 22 02.931 +11 47 06.06 23.5G 531040 F51 C~2rXr 2014 02 28.30193 09 21 28.001 +11 50 33.82 22.5w 531040 F51 C~1w3p 2014 02 28.31491 09 21 27.963 +11 50 34.15 22.5w 531040 F51 C~1w3p 2014 02 28.34114 09 21 27.855 +11 50 34.91 22.5w 531040 F51 C~1w3p 2014 03 20.27162 09 20 11.945 +11 58 41.78 22.8w 531040 F51 C~1w3p 2014 03 24.26564 09 19 59.449 +12 00 09.98 22.3w 531040 F51 C~1w3p 2014 05 25.27677 09 19 32.625 +12 10 55.95 22.5G 531040 F51 C~2rXr 2014 11 26.58207 09 32 09.111 +11 19 44.00 23.2G 531040 F51 C~2rXr 2014 12 18.51333 09 31 38.014 +11 22 05.93 22.0G 531040 F51 C~2rXr 2015 01 20.54479 09 29 44.203 +11 31 55.40 22.4G 531040 F51 C~2rXr 2015 01 22.55512 09 29 35.496 +11 32 42.58 22.6G 531040 F51 C~2rXr 2015 01 22.56743 09 29 35.433 +11 32 42.81 23.2G 531040 F51 C~2rXr 2015 01 22.57972 09 29 35.383 +11 32 43.02 22.9G 531040 F51 C~2rXr 2015 01 22.59203 09 29 35.324 +11 32 43.35 22.3G 531040 F51 C~2rXr 2015 03 18.24234 09 25 38.166 +11 56 02.84 22.7G 531040 F51 C~2rXr 2015 03 18.25458 09 25 38.132 +11 56 03.15 22.5G 531040 F51 C~2rXr 2015 03 18.26671 09 25 38.074 +11 56 03.48 22.4G 531040 F51 C~2rXr 2015 03 19.40717 09 25 34.157 +11 56 29.75 22.7G 531040 F51 C~2rXr 2016 01 15.57037 09 35 25.439 +11 27 28.46 22.6G 531040 F51 C~2rXr 2016 01 17.43559 09 35 17.859 +11 28 09.97 22.4G 531040 F51 C~2rXr 2016 02 01.41562 09 34 12.523 +11 34 13.85 22.1G 531040 F51 C~2rXr 2016 02 28.35186 09 32 09.679 +11 46 13.34 22.7G 531040 F51 C~2rXr 2016 03 07.29167 09 31 36.183 +11 49 40.97 22.6G 531040 F51 C~2rXr 2016 04 04.38128 09 30 04.192 +12 00 12.55 23.0G 531040 F51 C~2rXr 2017 02 18.61184 09 38 10.407 +11 39 31.06 22.6G 531040 F51 C~2rXr 2017 02 21.33858 09 37 58.000 +11 40 45.37 22.4G 531040 F51 C~2rXr 2017 03 27.36997 09 35 44.681 +11 55 00.44 22.2G 531040 F51 C~2rXr 2018 01 16.42100 09 45 59.130 +11 21 54.98 22.4G 531040 F51 C~2rXr 2018 01 16.42962 09 45 59.086 +11 21 55.19 22.4G 531040 F51 C~2rXr 2018 01 16.43283 09 45 59.076 +11 21 55.10 22.6G 531040 F51 C~2rXs 2018 01 16.44148 09 45 59.050 +11 21 55.56 22.5G 531040 F51 C~2rXs 2018 01 16.44471 09 45 59.032 +11 21 55.54 22.5G 531040 F51 C~2rXs 2018 01 16.45332 09 45 59.006 +11 21 55.67 23.1G 531040 F51 C~2rXs 2018 01 16.45656 09 45 58.987 +11 21 55.70 22.8G 531040 F51 C~2rXs 2018 03 07.24291 09 42 18.675 +11 43 55.75 23.0G 531040 F51 C~2rXs 2018 03 07.25453 09 42 18.636 +11 43 55.99 22.2G 531040 F51 C~2rXs 2018 03 07.26616 09 42 18.567 +11 43 56.50 22.6G 531040 F51 C~2rXs 2018 03 07.27778 09 42 18.548 +11 43 56.58 22.4G 531040 F51 C~2rXs 2018 03 17.27977 09 41 38.917 +11 48 11.86 22.9G 531040 F51 C~2rXs 2020 01 23.43417 09 56 12.186 +11 17 08.16 22.4w 531040 F51 C~3i3J 2020 01 23.44569 09 56 12.127 +11 17 08.54 22.2w 531040 F51 C~3i3J 2020 01 23.45731 09 56 12.091 +11 17 09.01 22.3w 531040 F51 C~3i3J 2022 03 02.234740 10 04 02.230 +11 26 26.34 22.6G 531040 G37 C~5V3d 2022 03 02.290870 10 04 01.958 +11 26 26.78 531040 G37 C~5V3d 2022 03 02.344910 10 04 01.739 +11 26 28.99 531040 G37 C~5V3d
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 0.64 0.00 -0.44
2 0.0000 0.00 0.53 0.00 -0.45
3 0.7426 0.00 -0.62 0.00 0.21
4 0.7426 0.00 -0.59 0.00 0.21
5 0.7426 0.00 -0.65 0.00 0.19
6 5.9010 0.00 -0.34 0.00 -0.27
7 5.9010 0.00 0.45 0.00 -0.02
8 5.9011 0.00 0.18 0.00 0.18
9 5.9011 0.00 0.19 0.00 0.26
10 5.9034 0.00 0.30 0.00 -0.03
11 5.9034 0.00 0.14 0.00 0.32
12 5.9037 0.00 -0.01 0.00 -0.16
13 6.9032 0.00 -0.14 0.00 -0.39
14 6.9033 0.00 0.31 0.00 -0.39
15 6.9549 0.00 -0.04 0.00 0.09
16 6.9550 0.00 0.04 0.00 0.12
17 7.9047 0.00 -0.09 0.00 0.01
18 7.9047 0.00 -0.04 0.00 -0.01
19 7.9048 0.00 0.22 0.00 -0.20
20 7.9811 0.00 0.04 0.00 -0.05
21 7.9811 0.00 0.09 0.00 0.03
22 7.9812 0.00 -0.04 0.00 -0.16
23 7.9812 0.00 0.01 0.00 0.03
24 8.6583 0.00 0.10 0.00 0.64
25 8.8249 0.00 0.08 0.00 -0.50
26 8.8249 0.00 0.11 0.00 0.34
27 8.8250 0.00 -0.06 0.00 0.05
28 8.8795 0.00 -0.19 0.00 -0.09
29 8.8795 0.00 -0.10 0.00 0.08
30 8.8795 0.00 0.22 0.00 -0.03
31 8.9506 0.00 -0.03 0.00 0.10
32 8.9723 0.00 -0.20 0.00 0.23
33 8.9723 0.00 0.08 0.00 0.23
34 8.9724 0.00 0.17 0.00 0.31
35 9.0270 0.00 0.09 0.00 0.10
36 9.0379 0.00 -0.15 0.00 0.34
37 9.2077 0.00 -0.15 0.00 -0.12
38 9.7150 0.00 -0.04 0.00 -0.17
39 9.7751 0.00 0.28 0.00 -0.42
40 9.8655 0.00 0.10 0.00 -0.08
41 9.8710 0.00 0.13 0.00 0.10
42 9.8710 0.00 0.01 0.00 0.04
43 9.8711 0.00 0.07 0.00 -0.04
44 9.8711 0.00 0.01 0.00 -0.00
45 10.0207 0.00 -0.09 0.00 0.20
46 10.0208 0.00 0.05 0.00 0.22
47 10.0208 0.00 -0.17 0.00 0.26
48 10.0239 0.00 0.07 0.00 0.06
49 10.8512 0.00 0.05 0.00 -0.04
50 10.8563 0.00 0.01 0.00 -0.08
51 10.8973 0.00 -0.23 0.00 -0.04
52 10.9711 0.00 -0.01 0.00 0.01
53 10.9928 0.00 -0.11 0.00 -0.04
54 11.0697 0.00 -1.27 0.00 0.09
55 11.9465 0.00 0.08 0.00 0.08
56 11.9539 0.00 0.01 0.00 -0.23
57 12.0471 0.00 -0.09 0.00 0.17
58 12.8549 0.00 0.03 0.00 -0.03
59 12.8549 0.00 -0.11 0.00 -0.02
60 12.8549 0.00 -0.07 0.00 -0.18
61 12.8550 0.00 0.06 0.00 0.08
62 12.8550 0.00 -0.01 0.00 -0.02
63 12.8550 0.00 0.12 0.00 -0.09
64 12.8550 0.00 0.03 0.00 -0.13
65 12.9913 0.00 -0.13 0.00 -0.08
66 12.9913 0.00 0.03 0.00 -0.15
67 12.9914 0.00 -0.27 0.00 0.05
68 12.9914 0.00 0.18 0.00 -0.18
69 13.0188 0.00 0.09 0.00 0.08
70 14.8727 0.00 0.32 0.00 -0.10
71 14.8728 0.00 0.16 0.00 -0.01
72 14.8728 0.00 0.35 0.00 0.17
73 16.9776 0.00 -0.09 0.00 0.49
74 16.9778 0.00 -0.35 0.00 -0.67
75 16.9779 0.00 0.03 0.00 0.00
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.
531040 quality flag:3 Type: SCATEXTD SCATEXTD SCATEXTD axisobj 43.386 43.386 43.387 ecceobj 0.030 0.030 0.030 incobj 17.044 17.044 17.044 qmin 41.391 41.391 41.401 qmax 45.508 45.510 45.507 amean 43.373 43.373 43.373 amin 43.050 43.046 43.046 amax 43.704 43.705 43.705 emean 0.031 0.031 0.031 emin 0.020 0.020 0.020 emax 0.042 0.042 0.042 imean 16.143 16.143 16.143 imin 15.727 15.728 15.725 imax 16.570 16.569 16.570 excite_mean 0.280 0.280 0.280 fracstop 1.000 1.000 1.000 cjmean 2.999 2.999 2.999 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 176.7 176.8 176.7 kozaiamp 179.9 180.0 180.0