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: 533028
# Created Sat Apr 27 01:08:39 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 137 observations of 137
# Arc: 13.62y
# First observation: 2010/05/12
# Last observation: 2023/12/24
# Chi-squared of fit: 116.76 DOF: 268 RMS: 0.16
# Min/Max residuals: -1.04 0.56
# Exact a, adot, b, bdot, g, gdot:
1.733484E-05 2.913499E-02 2.506242E-06 2.171554E-03 2.685031E-02 -6.504891E-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
0.904544 115.400826 -0.911593 -0.006944 0.437272 2455328.762656
# Heliocentric elements and errors
Epoch: 2455328.5000 = 2010/05/12
Mean Anomaly: 320.12074 +/- 0.000
Argument of Peri: 74.92183 +/- 0.000
Long of Asc Node: 104.61289 +/- 0.000
Inclination: 4.32204 +/- 0.000
Eccentricity: 0.24497772 +/- 0.0000
Semi-Major Axis: 43.56697426 +/- 0.0000
Time of Perihelion: 2466963.8406 +/- 0.0
Perihelion: 32.89403619 +/- 0.0000
Aphelion: 54.23991233 +/- 0.0000
Period (y) 287.5705 +/- 0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -16.60595197 +/- 0.0000
Ecliptic Y 32.85044124 +/- 0.0000
Ecliptic Z 0.58807075 +/- 0.0000
Ecliptic XDOT -0.00239592 +/- 0.0000
Ecliptic YDOT -0.00187060 +/- 0.0000
Ecliptic ZDOT 0.00021089 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 36.81391301 +/- 0.0000
Geocenter to KBO 37.24370065 +/- 0.0000
# Hcoef: 6.56
The following table shows the complete astrometric record for 533028. 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 (533028) followed by the observatory code and reference code for the source of the astrometry.
2010 05 12.26189 07 50 10.225 +21 56 52.33 22.4G 533028 F51 C~2qbC 2010 05 12.27056 07 50 10.289 +21 56 52.37 22.7G 533028 F51 C~2qbC 2011 01 25.35040 08 00 32.876 +21 36 21.96 22.7G 533028 F51 C~2qbC 2011 01 26.32223 08 00 27.194 +21 36 38.92 22.4G 533028 F51 C~2qbC 2011 01 30.29461 08 00 04.314 +21 37 47.84 22.4w 533028 F51 C~1vXA 2011 01 30.30913 08 00 04.245 +21 37 48.07 22.4w 533028 F51 C~1vXA 2011 01 30.32420 08 00 04.157 +21 37 48.31 22.1w 533028 F51 C~1vXA 2011 01 30.33857 08 00 04.066 +21 37 48.57 22.3w 533028 F51 C~1vXA 2012 01 26.50190 08 08 00.738 +21 22 28.17 21.7i 533028 F51 C~1vXA 2012 01 26.51481 08 08 00.645 +21 22 28.62 21.6i 533028 F51 C~1vXA 2012 01 26.53988 08 08 00.513 +21 22 29.07 21.7r 533028 F51 C~1vXA 2013 01 21.51592 08 16 03.033 +21 05 25.88 22.0G 533028 F51 C~2qbC 2013 02 12.28932 08 13 59.114 +21 12 18.16 21.2G 533028 F51 C~2qbC 2013 02 12.30250 08 13 59.049 +21 12 18.29 22.4G 533028 F51 C~2qbC 2013 02 12.31573 08 13 58.968 +21 12 18.42 22.2G 533028 F51 C~2qbC 2013 02 12.32895 08 13 58.898 +21 12 19.21 21.2G 533028 F51 C~2qbC 2014 01 01.41109 08 25 39.336 +20 41 06.39 22.2w 533028 F51 C~1vXA 2014 01 01.42492 08 25 39.282 +20 41 06.79 22.0w 533028 F51 C~1vXA 2014 01 01.43877 08 25 39.203 +20 41 06.84 22.4w 533028 F51 C~1vXB 2014 01 01.45276 08 25 39.125 +20 41 07.27 22.1w 533028 F51 C~1vXB 2014 01 10.57229 08 24 49.226 +20 44 16.09 22.8G 533028 F51 C~2qbC 2014 02 23.25971 08 20 44.766 +20 58 35.23 21.8w 533028 F51 C~1vXB 2014 02 23.28482 08 20 44.624 +20 58 35.45 21.8w 533028 F51 C~1vXB 2014 02 23.29747 08 20 44.568 +20 58 35.50 22.0w 533028 F51 C~1vXB 2014 02 26.39897 08 20 29.928 +20 59 24.04 22.4w 533028 F51 C~1vXB 2014 02 26.41202 08 20 29.867 +20 59 24.11 22.6w 533028 F51 C~1vXB 2014 02 26.42502 08 20 29.778 +20 59 23.94 22.3w 533028 F51 C~1vXB 2014 02 26.43804 08 20 29.741 +20 59 24.35 22.1w 533028 F51 C~1vXB 2014 03 06.40273 08 19 55.470 +21 01 14.77 22.3w 533028 F51 C~1vXB 2014 03 06.41576 08 19 55.409 +21 01 14.67 22.4w 533028 F51 C~1vXB 2014 03 06.42883 08 19 55.394 +21 01 15.04 22.0w 533028 F51 C~1vXB 2014 03 06.44191 08 19 55.302 +21 01 15.46 22.3w 533028 F51 C~1vXB 2014 05 20.25979 08 19 55.179 +21 00 00.79 22.1G 533028 F51 C~2qbC 2014 12 21.59272 08 34 16.469 +20 18 23.76 22.2w 533028 F51 C~1vXB 2014 12 21.60628 08 34 16.413 +20 18 23.87 22.2w 533028 F51 C~1vXB 2014 12 21.62002 08 34 16.346 +20 18 24.31 22.4w 533028 F51 C~1vXB 2014 12 21.63381 08 34 16.271 +20 18 24.47 22.1w 533028 F51 C~1vXB 2015 01 14.37428 08 32 13.927 +20 26 41.08 22.1w 533028 F51 C~1vXB 2015 01 14.38661 08 32 13.851 +20 26 41.45 21.9w 533028 F51 C~1vXB 2015 01 14.39884 08 32 13.782 +20 26 41.64 22.2w 533028 F51 C~1vXB 2015 01 14.41107 08 32 13.698 +20 26 41.90 22.4w 533028 F51 C~1vXB 2015 01 16.54218 08 32 01.500 +20 27 29.20 22.2G 533028 F51 C~2qbC 2015 01 16.55446 08 32 01.429 +20 27 29.54 22.0G 533028 F51 C~2qbC 2015 01 16.56675 08 32 01.355 +20 27 29.82 21.9G 533028 F51 C~2qbC 2015 02 16.28437 08 29 05.448 +20 38 20.30 21.8G 533028 F51 C~2qbC 2015 02 16.29668 08 29 05.367 +20 38 20.50 22.3G 533028 F51 C~2qbC 2015 02 16.30903 08 29 05.320 +20 38 20.53 22.9G 533028 F51 C~2qbC 2015 02 16.32142 08 29 05.244 +20 38 20.84 21.9G 533028 F51 C~2qbC 2015 02 17.28490 08 29 00.122 +20 38 39.01 21.9w 533028 F51 C~1vXB 2015 02 17.29650 08 29 00.048 +20 38 39.20 21.6G 533028 F51 C~2qbC 2015 02 17.29729 08 29 00.051 +20 38 39.23 22.0w 533028 F51 C~1vXB 2015 02 17.30885 08 28 59.980 +20 38 39.40 21.8G 533028 F51 C~2qbC 2015 02 17.30963 08 28 59.991 +20 38 39.67 22.1w 533028 F51 C~1vXB 2015 02 17.32131 08 28 59.911 +20 38 39.64 22.4G 533028 F51 C~2qbC 2015 02 17.32207 08 28 59.917 +20 38 39.69 21.7w 533028 F51 C~1vXB 2015 03 16.37090 08 27 01.512 +20 45 19.55 22.1w 533028 F51 C~1vXB 2015 03 16.38321 08 27 01.475 +20 45 19.75 22.1w 533028 F51 C~1vXB 2015 03 16.39549 08 27 01.419 +20 45 19.99 22.1w 533028 F51 C~1vXB 2015 03 16.40769 08 27 01.379 +20 45 19.90 22.0w 533028 F51 C~1vXB 2015 03 17.37223 08 26 58.294 +20 45 29.72 22.2G 533028 F51 C~2qbC 2015 03 17.38481 08 26 58.260 +20 45 29.88 21.8G 533028 F51 C~2qbC 2015 04 10.29948 08 26 12.893 +20 47 37.59 22.3w 533028 F51 C~1vXB 2015 04 10.31129 08 26 12.885 +20 47 37.60 22.2w 533028 F51 C~1vXB 2015 04 10.32306 08 26 12.874 +20 47 37.56 22.1w 533028 F51 C~1vXB 2015 04 10.33489 08 26 12.871 +20 47 37.60 22.1w 533028 F51 C~1vXB 2015 10 24.57206 08 43 15.863 +19 49 17.70 21.7G 533028 F51 C~2qbC 2015 10 24.57530 08 43 15.863 +19 49 17.71 22.2G 533028 F51 C~2qbC 2015 10 24.57854 08 43 15.868 +19 49 17.74 22.4G 533028 F51 C~2qbC 2015 10 24.58177 08 43 15.869 +19 49 17.64 22.3G 533028 F51 C~2qbC 2016 01 07.39166 08 40 41.610 +20 03 36.07 22.2G 533028 F51 C~2qbC 2016 01 07.40414 08 40 41.546 +20 03 36.23 22.3G 533028 F51 C~2qbC 2016 01 07.41659 08 40 41.489 +20 03 36.47 22.6G 533028 F51 C~2qbC 2016 01 07.42909 08 40 41.397 +20 03 36.92 22.4G 533028 F51 C~2qbC 2016 01 29.50289 08 38 35.729 +20 12 04.98 21.7G 533028 F51 C~2qbC 2016 02 11.28249 08 37 21.995 +20 16 47.77 21.9G 533028 F51 C~2qbC 2016 03 03.23882 08 35 34.600 +20 23 19.57 22.1G 533028 F51 C~2qbC 2016 03 03.25047 08 35 34.545 +20 23 19.79 22.1G 533028 F51 C~2qbC 2016 03 03.26396 08 35 34.481 +20 23 20.02 21.6G 533028 F51 C~2qbC 2016 03 03.27564 08 35 34.421 +20 23 20.23 21.9G 533028 F51 C~2qbC 2016 04 21.28753 08 33 50.745 +20 28 32.27 22.2G 533028 F51 C~2qbC 2016 04 28.26022 08 33 57.624 +20 27 55.91 21.9G 533028 F51 C~2qbC 2016 04 28.27281 08 33 57.654 +20 27 55.78 22.3G 533028 F51 C~2qbC 2016 04 28.28543 08 33 57.676 +20 27 55.75 22.0G 533028 F51 C~2qbC 2016 05 02.26729 08 34 04.115 +20 27 26.11 22.1G 533028 F51 C~2qbC 2016 05 02.27922 08 34 04.140 +20 27 25.69 21.6G 533028 F51 C~2qbC 2016 11 08.55419 08 51 12.934 +19 27 18.18 22.3G 533028 F51 C~2qbC 2017 01 28.52937 08 46 28.221 +19 50 23.98 21.8G 533028 F51 C~2qbC 2017 02 16.202214 08 44 41.27 +19 57 29.3 22.2V 533028 H21 C~27xm 2017 02 16.215825 08 44 41.18 +19 57 29.9 22.2V 533028 H21 C~27xm 2017 02 16.232683 08 44 41.05 +19 57 30.7 22.5V 533028 H21 C~27xm 2017 02 27.28376 08 43 43.498 +20 01 10.08 22.3G 533028 F51 C~2qbC 2017 11 20.59010 08 58 53.761 +19 04 52.74 22.9G 533028 F51 C~2qbC 2017 12 04.52677 08 58 32.661 +19 07 22.65 21.9G 533028 F51 C~2qbC 2017 12 10.49650 08 58 17.145 +19 08 52.29 23.3G 533028 F51 C~2qbC 2017 12 11.52127 08 58 14.112 +19 09 08.80 21.7G 533028 F51 C~2qbC 2017 12 12.53797 08 58 10.973 +19 09 26.18 20.6G 533028 F51 C~2qbC 2017 12 23.47196 08 57 31.163 +19 12 51.99 22.0G 533028 F51 C~2qbC 2017 12 23.58552 08 57 30.701 +19 12 54.41 21.8G 533028 F51 C~2qbC 2017 12 23.59748 08 57 30.653 +19 12 54.63 21.8G 533028 F51 C~2qbC 2017 12 23.60943 08 57 30.605 +19 12 54.96 22.3G 533028 F51 C~2qbC 2017 12 23.62138 08 57 30.549 +19 12 55.10 22.0G 533028 F51 C~2qbC 2017 12 25.46609 08 57 22.783 +19 13 33.66 21.8G 533028 F51 C~2qbC 2017 12 26.61424 08 57 17.807 +19 13 58.15 21.9G 533028 F51 C~2qbC 2017 12 31.44510 08 56 55.803 +19 15 44.54 21.8G 533028 F51 C~2qbC 2018 01 07.60474 08 56 20.280 +19 18 31.35 22.1G 533028 F51 C~2qbC 2018 01 09.42502 08 56 10.805 +19 19 15.11 21.6G 533028 F51 C~2qbC 2018 01 15.40641 08 55 38.420 +19 21 41.89 22.6G 533028 F51 C~2qbC 2018 01 16.35368 08 55 33.160 +19 22 05.47 22.0G 533028 F51 C~2qbC 2018 01 16.36530 08 55 33.094 +19 22 05.82 21.9G 533028 F51 C~2qbC 2018 01 16.37700 08 55 33.033 +19 22 06.01 22.0G 533028 F51 C~2qbC 2018 01 16.38860 08 55 32.957 +19 22 06.32 22.1G 533028 F51 C~2qbC 2018 02 03.33883 08 53 49.452 +19 29 35.67 21.5G 533028 F51 C~2qbC 2018 02 12.46967 08 52 56.768 +19 33 14.60 22.8G 533028 F51 C~2qbC 2018 02 12.48145 08 52 56.685 +19 33 14.60 22.0G 533028 F51 C~2qbC 2018 02 12.49324 08 52 56.623 +19 33 14.95 22.4G 533028 F51 C~2qbC 2018 02 12.50524 08 52 56.549 +19 33 15.16 21.9G 533028 F51 C~2qbC 2019 01 14.57890 09 03 39.447 +18 56 25.24 22.4w 533028 F51 C~4fM6 2019 01 14.59256 09 03 39.318 +18 56 26.14 22.4w 533028 F51 C~4fM6 2019 01 14.60617 09 03 39.302 +18 56 25.88 22.3w 533028 F51 C~4fM6 2021 11 11.562038 09 29 57.140 +17 16 31.08 21.8w 533028 F52 C~5IvR 2021 11 11.574715 09 29 57.190 +17 16 31.33 21.8w 533028 F52 C~5IvR 2021 11 11.587398 09 29 57.199 +17 16 30.99 21.9w 533028 F52 C~5IvR 2022 02 03.332595 09 25 45.914 +17 42 25.34 21.5w 533028 F52 C~5V3h 2022 02 03.345256 09 25 45.853 +17 42 25.85 21.7w 533028 F52 C~5V3h 2022 02 03.357911 09 25 45.753 +17 42 26.11 21.7w 533028 F52 C~5V3h 2022 02 09.343161 09 25 11.081 +17 45 16.73 21.7w 533028 F52 C~5V3h 2022 02 09.355256 09 25 11.022 +17 45 17.22 21.6w 533028 F52 C~5V3h 2022 02 09.367299 09 25 10.946 +17 45 17.52 21.8w 533028 F52 C~5V3h 2022 03 02.292921 09 23 13.677 +17 54 28.30 21.6w 533028 F52 C~5V3h 2022 03 02.317090 09 23 13.556 +17 54 29.17 21.8w 533028 F52 C~5V3h 2022 03 02.329303 09 23 13.482 +17 54 29.31 21.8w 533028 F52 C~5V3h 2023 11 19.90424 09 45 47.05 +16 14 19.5 22.2w 533028 O18 C~7b1g 2023 11 19.90852 09 45 47.05 +16 14 19.5 22.0w 533028 O18 C~7b1g 2023 11 19.91287 09 45 47.06 +16 14 19.3 22.1w 533028 O18 C~7b1g 2023 12 24.621142 09 45 07.410 +16 21 06.35 21.8w 533028 F51 C~7gdT 2023 12 24.632884 09 45 07.378 +16 21 06.78 21.8w 533028 F51 C~7gdT 2023 12 24.644666 09 45 07.344 +16 21 06.86 21.8w 533028 F51 C~7gdT
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 -0.09 0.00 -0.24
2 0.0000 0.00 0.36 0.00 -0.11
3 0.7066 0.00 0.37 0.00 0.11
4 0.7093 0.00 -0.23 0.00 0.00
5 0.7201 0.00 -0.15 0.00 0.08
6 0.7202 0.00 0.08 0.00 0.05
7 0.7202 0.00 0.07 0.00 0.03
8 0.7203 0.00 -0.04 0.00 0.04
9 1.7091 0.00 0.14 0.00 -0.21
10 1.7091 0.00 -0.11 0.00 0.00
11 1.7092 0.00 0.13 0.00 -0.00
12 2.6975 0.00 0.05 0.00 -0.14
13 2.7571 0.00 -0.17 0.00 0.08
14 2.7571 0.00 -0.07 0.00 -0.02
15 2.7572 0.00 -0.20 0.00 -0.12
16 2.7572 0.00 -0.17 0.00 0.44
17 3.6418 0.00 -0.09 0.00 -0.05
18 3.6418 0.00 0.21 0.00 0.07
19 3.6418 0.00 0.14 0.00 -0.17
20 3.6419 0.00 0.10 0.00 -0.02
21 3.6668 0.00 0.07 0.00 -0.31
22 3.7864 0.00 0.06 0.00 0.12
23 3.7865 0.00 -0.22 0.00 -0.07
24 3.7865 0.00 -0.12 0.00 -0.22
25 3.7950 0.00 0.02 0.00 0.32
26 3.7951 0.00 0.03 0.00 0.20
27 3.7951 0.00 -0.39 0.00 -0.16
28 3.7951 0.00 -0.02 0.00 0.05
29 3.8169 0.00 -0.18 0.00 0.18
30 3.8170 0.00 -0.30 0.00 -0.08
31 3.8170 0.00 0.27 0.00 0.13
32 3.8171 0.00 -0.31 0.00 0.39
33 4.0219 0.00 -0.13 0.00 -0.03
34 4.6114 0.00 0.08 0.00 0.07
35 4.6115 0.00 0.16 0.00 -0.07
36 4.6115 0.00 0.08 0.00 0.11
37 4.6116 0.00 -0.11 0.00 0.01
38 4.6766 0.00 0.08 0.00 -0.06
39 4.6766 0.00 0.01 0.00 0.03
40 4.6766 0.00 0.03 0.00 -0.05
41 4.6767 0.00 -0.17 0.00 -0.07
42 4.6825 0.00 -0.01 0.00 -0.07
43 4.6825 0.00 -0.00 0.00 -0.00
44 4.6826 0.00 -0.03 0.00 0.01
45 4.7667 0.00 0.11 0.00 0.11
46 4.7667 0.00 -0.10 0.00 0.07
47 4.7667 0.00 0.21 0.00 -0.13
48 4.7668 0.00 0.08 0.00 -0.06
49 4.7694 0.00 0.08 0.00 0.04
50 4.7694 0.00 -0.10 0.00 0.01
51 4.7694 0.00 0.01 0.00 0.03
52 4.7695 0.00 -0.12 0.00 -0.02
53 4.7695 0.00 0.11 0.00 0.23
54 4.7695 0.00 -0.15 0.00 -0.02
55 4.7695 0.00 0.00 0.00 0.02
56 4.8436 0.00 0.03 0.00 -0.03
57 4.8436 0.00 0.09 0.00 0.04
58 4.8436 0.00 -0.13 0.00 0.16
59 4.8437 0.00 -0.12 0.00 -0.05
60 4.8463 0.00 -0.03 0.00 -0.04
61 4.8463 0.00 0.08 0.00 0.00
62 4.9118 0.00 0.08 0.00 0.06
63 4.9118 0.00 0.08 0.00 0.06
64 4.9119 0.00 0.03 0.00 0.02
65 4.9119 0.00 0.10 0.00 0.05
66 5.4519 0.00 0.06 0.00 0.00
67 5.4519 0.00 -0.04 0.00 0.03
68 5.4519 0.00 -0.06 0.00 0.07
69 5.4519 0.00 -0.14 0.00 -0.02
70 5.6568 0.00 -0.03 0.00 0.07
71 5.6568 0.00 0.02 0.00 -0.05
72 5.6568 0.00 0.18 0.00 -0.09
73 5.6569 0.00 -0.18 0.00 0.07
74 5.7173 0.00 -0.19 0.00 -0.08
75 5.7523 0.00 -0.09 0.00 -0.14
76 5.8097 0.00 0.00 0.00 -0.03
77 5.8097 0.00 -0.03 0.00 0.00
78 5.8097 0.00 -0.06 0.00 0.02
79 5.8098 0.00 -0.16 0.00 0.04
80 5.9439 0.00 -0.08 0.00 0.00
81 5.9630 0.00 -0.12 0.00 0.03
82 5.9631 0.00 0.09 0.00 -0.02
83 5.9631 0.00 0.17 0.00 0.04
84 5.9740 0.00 0.02 0.00 0.20
85 5.9740 0.00 0.07 0.00 -0.12
86 6.4950 0.00 -0.11 0.00 0.11
87 6.7167 0.00 -0.04 0.00 0.05
88 6.7678 0.00 0.56 0.00 -1.04
89 6.7678 0.00 0.34 0.00 -0.73
90 6.7679 0.00 -0.20 0.00 -0.28
91 6.7981 0.00 0.01 0.00 0.03
92 7.5273 0.00 -0.02 0.00 0.05
93 7.5654 0.00 -0.17 0.00 -0.07
94 7.5818 0.00 0.22 0.00 -0.00
95 7.5846 0.00 0.36 0.00 -0.28
96 7.5873 0.00 0.12 0.00 0.06
97 7.6173 0.00 -0.34 0.00 -0.04
98 7.6176 0.00 -0.06 0.00 0.03
99 7.6176 0.00 -0.01 0.00 0.01
100 7.6177 0.00 0.02 0.00 0.09
101 7.6177 0.00 -0.06 0.00 -0.01
102 7.6227 0.00 -0.18 0.00 0.06
103 7.6259 0.00 0.05 0.00 0.12
104 7.6391 0.00 0.01 0.00 0.13
105 7.6587 0.00 0.06 0.00 0.16
106 7.6637 0.00 0.26 0.00 0.11
107 7.6801 0.00 -0.02 0.00 0.01
108 7.6827 0.00 -0.03 0.00 0.03
109 7.6827 0.00 -0.04 0.00 0.08
110 7.6827 0.00 0.04 0.00 -0.02
111 7.6828 0.00 -0.12 0.00 -0.01
112 7.7319 0.00 -0.24 0.00 0.28
113 7.7569 0.00 0.16 0.00 0.17
114 7.7569 0.00 -0.06 0.00 -0.10
115 7.7570 0.00 0.03 0.00 -0.02
116 7.7570 0.00 -0.04 0.00 -0.09
117 8.6771 0.00 0.25 0.00 -0.11
118 8.6772 0.00 -0.55 0.00 0.44
119 8.6772 0.00 0.33 0.00 -0.16
120 11.5025 0.00 -0.25 0.00 0.01
121 11.5026 0.00 0.26 0.00 0.26
122 11.5026 0.00 0.16 0.00 -0.08
123 11.7319 0.00 -0.07 0.00 -0.06
124 11.7319 0.00 0.13 0.00 0.08
125 11.7320 0.00 -0.26 0.00 -0.02
126 11.7483 0.00 -0.05 0.00 -0.04
127 11.7484 0.00 0.13 0.00 0.11
128 11.7484 0.00 0.05 0.00 0.06
129 11.8057 0.00 0.03 0.00 -0.11
130 11.8058 0.00 0.16 0.00 0.18
131 11.8058 0.00 0.03 0.00 0.03
132 13.5240 0.00 -0.13 0.00 -0.04
133 13.5240 0.00 -0.18 0.00 -0.05
134 13.5240 0.00 -0.08 0.00 -0.26
135 13.6191 0.00 0.00 0.00 -0.06
136 13.6191 0.00 0.08 0.00 0.13
137 13.6191 0.00 0.12 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.
533028 quality flag:3 Type: 7:4EEE 7:4EEE 7:4EEE axisobj 43.844 43.844 43.844 ecceobj 0.246 0.246 0.246 incobj 4.315 4.315 4.315 qmin 32.305 32.305 32.305 qmax 55.680 55.680 55.680 amean 43.726 43.726 43.726 amin 43.308 43.308 43.307 amax 44.223 44.221 44.225 emean 0.227 0.227 0.227 emin 0.181 0.181 0.181 emax 0.260 0.260 0.260 imean 5.858 5.860 5.857 imin 2.487 2.487 2.487 imax 9.247 9.248 9.246 excite_mean 0.253 0.253 0.253 fracstop 1.000 1.000 1.000 cjmean 3.021 3.021 3.021 libcent 0 181.9 182.6 180.8 libamp 0 56.0 56.9 54.4 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 95.9 95.9 96.0 kozaiamp 180.0 180.0 180.0