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: 555758
# Created Fri Nov 22 02:07:34 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 114 observations of 114
# Arc: 11.20y
# First observation: 2011/04/12
# Last observation: 2022/06/23
# Chi-squared of fit: 122.27 DOF: 222 RMS: 0.18
# Min/Max residuals: -0.74 0.51
# Exact a, adot, b, bdot, g, gdot:
1.769087E-05 3.888513E-02 9.311933E-06 1.744544E-02 3.399373E-02 -5.262519E-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
0.007401 -158.013912 0.001857 0.000087 -1.006053 2455663.885216
# Heliocentric elements and errors
Epoch: 2455664.5000 = 2011/04/13
Mean Anomaly: 338.92316 +/- 0.000
Argument of Peri: 35.82753 +/- 0.000
Long of Asc Node: 201.96940 +/- 0.000
Inclination: 24.20567 +/- 0.000
Eccentricity: 0.25555798 +/- 0.0000
Semi-Major Axis: 39.29003789 +/- 0.0000
Time of Perihelion: 2460931.0371 +/- 0.0
Perihelion: 29.24915501 +/- 0.0000
Aphelion: 49.33092077 +/- 0.0000
Period (y) 246.2815 +/- 0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -28.20716052 +/- 0.0000
Ecliptic Y -11.38875457 +/- 0.0000
Ecliptic Z 0.00410262 +/- 0.0000
Ecliptic XDOT 0.00156394 +/- 0.0000
Ecliptic YDOT -0.00273933 +/- 0.0000
Ecliptic ZDOT 0.00140503 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 30.41959927 +/- 0.0000
Geocenter to KBO 29.41729707 +/- 0.0000
# Hcoef: 7.53
The following table shows the complete astrometric record for 555758. 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 (555758) followed by the observatory code and reference code for the source of the astrometry.
2011 04 12.38445 13 21 18.916 -08 33 27.00 21.7G 555758 F51 C~2rY0 2011 04 12.39834 13 21 18.817 -08 33 26.11 22.4G 555758 F51 C~2rY0 2011 04 23.46731 13 20 13.998 -08 25 01.78 22.4G 555758 F51 C~2rY0 2011 05 01.33996 13 19 29.596 -08 19 12.59 21.7G 555758 F51 C~2rY0 2012 04 13.40625 13 31 02.609 -08 25 43.88 21.0G 555758 F51 C~2rY0 2013 04 10.42100 13 41 21.802 -08 20 49.07 22.3G 555758 F51 C~2rY0 2013 04 10.43463 13 41 21.718 -08 20 48.34 22.5G 555758 F51 C~2rY0 2013 04 10.44830 13 41 21.629 -08 20 47.56 23.0G 555758 F51 C~2rY0 2013 04 10.46202 13 41 21.542 -08 20 47.25 22.5G 555758 F51 C~2rY0 2013 04 19.47008 13 40 27.830 -08 14 00.92 22.4G 555758 F51 C~2rY0 2013 04 19.48156 13 40 27.758 -08 14 00.80 22.8G 555758 F51 C~2rY0 2014 02 25.57129 13 54 53.341 -08 41 55.05 22.2w 555758 F51 C~1vXI 2014 02 25.59651 13 54 53.269 -08 41 54.38 22.3w 555758 F51 C~1vXI 2014 02 25.60909 13 54 53.224 -08 41 53.67 22.5w 555758 F51 C~1vXI 2014 03 04.53838 13 54 31.323 -08 38 04.56 22.4G 555758 F51 C~2rY0 2014 03 04.55129 13 54 31.305 -08 38 03.81 22.0G 555758 F51 C~2rY0 2014 04 04.44976 13 52 03.486 -08 17 06.93 22.1w 555758 F51 C~1vXI 2014 04 04.46113 13 52 03.427 -08 17 06.35 22.3w 555758 F51 C~1vXI 2014 04 04.47249 13 52 03.358 -08 17 05.72 22.2w 555758 F51 C~1vXI 2014 04 04.48384 13 52 03.262 -08 17 05.13 22.5w 555758 F51 C~1vXI 2014 04 28.44007 13 49 41.047 -07 59 21.80 22.1w 555758 F51 C~1vXI 2014 04 28.45301 13 49 40.967 -07 59 21.59 22.2w 555758 F51 C~1vXI 2014 04 28.46590 13 49 40.899 -07 59 20.97 22.2w 555758 F51 C~1vXI 2014 05 20.33456 13 47 40.187 -07 44 57.28 22.3G 555758 F51 C~2rY0 2014 05 20.34752 13 47 40.127 -07 44 56.90 22.5G 555758 F51 C~2rY0 2014 05 20.36045 13 47 40.056 -07 44 56.36 22.4G 555758 F51 C~2rY0 2014 05 20.37338 13 47 39.991 -07 44 56.22 22.5G 555758 F51 C~2rY0 2014 05 30.29754 13 46 54.572 -07 39 33.34 22.4G 555758 F51 C~2rY0 2014 05 30.30930 13 46 54.531 -07 39 33.03 22.5G 555758 F51 C~2rY0 2014 06 29.27570 13 45 33.583 -07 29 25.70 22.5w 555758 F51 C~1vXI 2014 06 29.28680 13 45 33.572 -07 29 25.80 22.9w 555758 F51 C~1vXI 2014 06 29.29790 13 45 33.556 -07 29 25.58 22.3w 555758 F51 C~1vXI 2014 06 29.30899 13 45 33.550 -07 29 25.58 22.7w 555758 F51 C~1vXI 2015 01 24.62403 14 05 12.593 -08 43 52.32 23.0G 555758 F51 C~2rY0 2015 01 24.63623 14 05 12.599 -08 43 51.90 22.7G 555758 F51 C~2rY0 2015 01 24.64842 14 05 12.617 -08 43 52.33 22.6G 555758 F51 C~2rY0 2015 01 26.60938 14 05 15.512 -08 43 30.46 22.4w 555758 F51 C~1vXI 2015 01 26.62136 14 05 15.532 -08 43 30.33 22.6w 555758 F51 C~1vXI 2015 01 26.63331 14 05 15.540 -08 43 29.96 22.4w 555758 F51 C~1vXI 2015 01 26.64531 14 05 15.552 -08 43 30.06 22.7w 555758 F51 C~1vXI 2015 01 28.61116 14 05 17.922 -08 43 06.08 23.1G 555758 F51 C~2rY0 2015 01 28.62341 14 05 17.929 -08 43 06.23 22.6G 555758 F51 C~2rY0 2015 01 28.63569 14 05 17.931 -08 43 05.85 22.7G 555758 F51 C~2rY0 2015 01 28.64798 14 05 17.952 -08 43 05.86 22.5G 555758 F51 C~2rY0 2015 01 30.58137 14 05 19.762 -08 42 39.07 22.5w 555758 F51 C~1vXI 2015 01 30.59348 14 05 19.772 -08 42 39.01 22.6w 555758 F51 C~1vXI 2015 01 30.60554 14 05 19.784 -08 42 38.73 22.2w 555758 F51 C~1vXI 2015 02 23.59333 14 05 01.923 -08 33 39.34 22.8G 555758 F51 C~2rY0 2015 02 23.60636 14 05 01.913 -08 33 38.88 22.8G 555758 F51 C~2rY0 2015 02 23.61941 14 05 01.860 -08 33 38.57 22.2G 555758 F51 C~2rY0 2015 02 23.63241 14 05 01.833 -08 33 38.33 22.6G 555758 F51 C~2rY0 2015 02 24.58154 14 04 59.665 -08 33 09.22 22.1w 555758 F51 C~1vXI 2015 02 24.59456 14 04 59.655 -08 33 08.69 22.3w 555758 F51 C~1vXI 2015 02 24.60757 14 04 59.608 -08 33 08.49 22.4w 555758 F51 C~1vXI 2015 02 24.62062 14 04 59.557 -08 33 07.89 22.4w 555758 F51 C~1vXI 2015 03 20.55889 14 03 32.939 -08 18 37.08 22.2G 555758 F51 C~2rY0 2015 03 21.51856 14 03 28.371 -08 17 57.13 22.4G 555758 F51 C~2rY0 2015 03 21.53125 14 03 28.277 -08 17 56.70 22.3G 555758 F51 C~2rY0 2015 03 21.54414 14 03 28.250 -08 17 56.34 22.4G 555758 F51 C~2rY0 2015 04 20.43359 14 00 41.116 -07 56 08.20 22.7G 555758 F51 C~2rY0 2015 04 20.44625 14 00 41.054 -07 56 08.17 22.1G 555758 F51 C~2rY0 2015 04 20.45886 14 00 40.995 -07 56 07.46 21.8G 555758 F51 C~2rY0 2015 04 20.47159 14 00 40.898 -07 56 06.92 22.5G 555758 F51 C~2rY0 2015 04 21.45645 14 00 34.948 -07 55 23.54 21.4G 555758 F51 C~2rY0 2015 04 21.46938 14 00 34.865 -07 55 23.11 21.9G 555758 F51 C~2rY0 2015 04 21.52005 14 00 34.548 -07 55 20.91 22.2G 555758 F51 C~2rY0 2015 04 21.53300 14 00 34.448 -07 55 20.50 20.3G 555758 F51 C~2rY0 2016 02 11.57204 14 15 22.993 -08 28 45.32 22.7G 555758 F51 C~2rY0 2016 02 11.58438 14 15 22.990 -08 28 44.90 22.4G 555758 F51 C~2rY0 2016 02 11.59679 14 15 22.992 -08 28 44.78 22.3G 555758 F51 C~2rY0 2016 02 11.60920 14 15 23.004 -08 28 44.36 22.7G 555758 F51 C~2rY0 2016 03 03.63416 14 14 46.966 -08 18 32.80 22.0G 555758 F51 C~2rY0 2016 03 03.63957 14 14 46.938 -08 18 32.52 21.8G 555758 F51 C~2rY0 2016 03 08.49000 14 14 31.324 -08 15 38.15 22.2G 555758 F51 C~2rY0 2016 03 31.49152 14 12 47.598 -08 00 00.08 21.8G 555758 F51 C~2rY0 2016 04 04.47357 14 12 25.810 -07 57 05.75 22.6G 555758 F51 C~2rY0 2016 04 04.48549 14 12 25.746 -07 57 05.13 22.7G 555758 F51 C~2rY0 2016 04 04.49736 14 12 25.657 -07 57 04.80 22.2G 555758 F51 C~2rY0 2016 04 04.50932 14 12 25.601 -07 57 04.23 22.8G 555758 F51 C~2rY0 2016 05 01.41750 14 09 45.517 -07 37 35.12 22.3G 555758 F51 C~2rY0 2016 05 01.43021 14 09 45.423 -07 37 34.56 21.8G 555758 F51 C~2rY0 2016 05 01.44289 14 09 45.343 -07 37 34.21 21.4G 555758 F51 C~2rY0 2016 05 01.45560 14 09 45.275 -07 37 33.61 21.8G 555758 F51 C~2rY0 2016 06 28.30027 14 05 32.260 -07 10 59.92 22.3G 555758 F51 C~2rY0 2016 06 28.33937 14 05 32.203 -07 10 59.63 22.6G 555758 F51 C~2rY0 2017 03 22.48933 14 23 51.434 -07 55 15.91 22.7G 555758 F51 C~2rY0 2017 04 26.43644 14 20 36.868 -07 30 04.63 21.7G 555758 F51 C~2rY0 2017 04 26.44892 14 20 36.772 -07 30 03.82 22.2G 555758 F51 C~2rY0 2017 04 26.46139 14 20 36.694 -07 30 03.40 22.1G 555758 F51 C~2rY0 2017 04 26.47385 14 20 36.614 -07 30 02.83 22.3G 555758 F51 C~2rY0 2017 05 02.32316 14 20 00.88 -07 26 00.3 21.7R 555758 G37 C~2Fa8 2017 05 02.39060 14 20 00.47 -07 25 57.6 555758 G37 C~2Fa8 2017 05 17.30564 14 18 32.302 -07 16 30.13 22.1G 555758 F51 C~2rY0 2017 05 17.31726 14 18 32.253 -07 16 29.56 22.3G 555758 F51 C~2rY0 2017 05 17.32893 14 18 32.172 -07 16 29.48 22.2G 555758 F51 C~2rY0 2017 05 17.34058 14 18 32.122 -07 16 29.20 21.9G 555758 F51 C~2rY0 2020 02 25.57892 14 56 00.868 -07 31 26.63 21.3w 555758 F52 C#02tw 2020 02 25.59014 14 56 00.835 -07 31 27.10 21.5w 555758 F52 C#02tw 2020 02 25.60142 14 56 00.770 -07 31 25.54 21.5w 555758 F52 C#02tw 2020 04 29.49978 14 51 34.247 -06 48 15.19 22.0w 555758 F51 C~3st6 2020 04 29.51198 14 51 34.178 -06 48 14.76 22.0w 555758 F51 C~3st6 2020 04 29.52421 14 51 34.084 -06 48 14.37 22.0w 555758 F51 C~3st6 2021 04 09.535391 15 04 01.014 -06 47 13.33 22.1w 555758 F51 C~4i1C 2021 04 09.547450 15 04 00.965 -06 47 12.65 22.2w 555758 F51 C~4i1C 2021 04 09.559473 15 04 00.862 -06 47 12.22 22.0w 555758 F51 C~4i1C 2021 04 09.573691 15 04 00.810 -06 47 11.67 21.8w 555758 F51 C~4i1C 2021 05 10.396565 15 00 57.781 -06 26 19.11 22.1w 555758 F51 C~4n4R 2021 05 10.408596 15 00 57.696 -06 26 18.41 21.9w 555758 F51 C~4n4R 2021 05 10.420571 15 00 57.631 -06 26 17.96 22.0w 555758 F51 C~4n4R 2021 05 10.432572 15 00 57.553 -06 26 17.80 22.1w 555758 F51 C~4n4R 2022 06 23.317256 15 07 25.633 -05 52 48.17 22.0w 555758 F52 C~5i0E 2022 06 23.329414 15 07 25.574 -05 52 48.23 22.1w 555758 F52 C~5i0E 2022 06 23.341508 15 07 25.534 -05 52 48.02 22.2w 555758 F52 C~5i0E 2022 06 23.353552 15 07 25.495 -05 52 48.03 22.2w 555758 F52 C~5i0E
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 -0.02 0.00 -0.26
2 0.0000 0.00 -0.25 0.00 -0.01
3 0.0303 0.00 -0.01 0.00 -0.17
4 0.0519 0.00 -0.52 0.00 0.18
5 1.0049 0.00 -0.17 0.00 -0.14
6 1.9960 0.00 0.17 0.00 -0.07
7 1.9960 0.00 0.14 0.00 0.04
8 1.9961 0.00 0.05 0.00 0.20
9 1.9961 0.00 -0.01 0.00 -0.11
10 2.0208 0.00 0.31 0.00 0.04
11 2.0208 0.00 0.28 0.00 -0.35
12 2.8753 0.00 0.08 0.00 -0.06
13 2.8753 0.00 0.10 0.00 -0.18
14 2.8754 0.00 -0.03 0.00 0.14
15 2.8943 0.00 -0.36 0.00 -0.09
16 2.8944 0.00 0.08 0.00 0.21
17 2.9790 0.00 0.06 0.00 -0.03
18 2.9790 0.00 0.17 0.00 0.05
19 2.9790 0.00 0.13 0.00 0.17
20 2.9791 0.00 -0.31 0.00 0.26
21 3.0446 0.00 0.10 0.00 0.30
22 3.0447 0.00 0.07 0.00 -0.05
23 3.0447 0.00 0.22 0.00 0.02
24 3.1046 0.00 -0.06 0.00 0.04
25 3.1046 0.00 0.02 0.00 -0.03
26 3.1047 0.00 -0.06 0.00 0.05
27 3.1047 0.00 -0.05 0.00 -0.26
28 3.1319 0.00 0.06 0.00 -0.10
29 3.1319 0.00 0.20 0.00 -0.14
30 3.2139 0.00 0.08 0.00 0.25
31 3.2140 0.00 0.11 0.00 0.03
32 3.2140 0.00 0.07 0.00 0.14
33 3.2140 0.00 0.17 0.00 0.03
34 3.7871 0.00 -0.06 0.00 -0.11
35 3.7871 0.00 -0.24 0.00 0.19
36 3.7872 0.00 -0.24 0.00 -0.36
37 3.7925 0.00 0.06 0.00 0.27
38 3.7926 0.00 0.14 0.00 0.26
39 3.7926 0.00 0.04 0.00 0.49
40 3.7926 0.00 0.00 0.00 0.26
41 3.7980 0.00 0.12 0.00 0.11
42 3.7981 0.00 0.05 0.00 -0.20
43 3.7981 0.00 -0.09 0.00 0.02
44 3.7981 0.00 0.05 0.00 -0.15
45 3.8034 0.00 -0.09 0.00 0.16
46 3.8034 0.00 -0.07 0.00 0.05
47 3.8035 0.00 -0.02 0.00 0.16
48 3.8692 0.00 -0.06 0.00 -0.06
49 3.8692 0.00 0.25 0.00 0.00
50 3.8692 0.00 -0.08 0.00 -0.08
51 3.8693 0.00 -0.02 0.00 -0.23
52 3.8719 0.00 0.16 0.00 0.08
53 3.8719 0.00 0.50 0.00 0.21
54 3.8719 0.00 0.28 0.00 0.01
55 3.8720 0.00 -0.00 0.00 0.21
56 3.9375 0.00 0.03 0.00 -0.28
57 3.9401 0.00 -0.02 0.00 0.04
58 3.9402 0.00 -0.50 0.00 -0.05
59 3.9402 0.00 0.05 0.00 -0.23
60 4.0220 0.00 -0.17 0.00 0.41
61 4.0221 0.00 0.07 0.00 -0.12
62 4.0221 0.00 0.35 0.00 0.03
63 4.0221 0.00 0.07 0.00 0.01
64 4.0248 0.00 0.08 0.00 0.09
65 4.0249 0.00 0.03 0.00 -0.04
66 4.0250 0.00 -0.04 0.00 -0.07
67 4.0250 0.00 -0.35 0.00 -0.23
68 4.8356 0.00 -0.16 0.00 -0.06
69 4.8356 0.00 -0.11 0.00 0.08
70 4.8356 0.00 0.01 0.00 -0.08
71 4.8357 0.00 0.29 0.00 0.05
72 4.8932 0.00 0.03 0.00 -0.09
73 4.8932 0.00 -0.14 0.00 0.00
74 4.9065 0.00 -0.02 0.00 0.27
75 4.9695 0.00 -0.08 0.00 -0.06
76 4.9804 0.00 0.12 0.00 -0.03
77 4.9804 0.00 0.18 0.00 0.06
78 4.9805 0.00 -0.14 0.00 -0.13
79 4.9805 0.00 0.04 0.00 -0.09
80 5.0542 0.00 0.09 0.00 0.10
81 5.0542 0.00 -0.14 0.00 0.14
82 5.0542 0.00 -0.17 0.00 -0.04
83 5.0543 0.00 -0.02 0.00 0.04
84 5.2126 0.00 -0.12 0.00 0.04
85 5.2127 0.00 0.12 0.00 -0.05
86 5.9442 0.00 -0.04 0.00 -0.10
87 6.0398 0.00 0.20 0.00 -0.23
88 6.0399 0.00 -0.07 0.00 0.06
89 6.0399 0.00 -0.07 0.00 -0.05
90 6.0399 0.00 -0.11 0.00 -0.01
91 6.0560 0.00 -0.09 0.00 0.03
92 6.0561 0.00 0.02 0.00 -0.02
93 6.0970 0.00 -0.46 0.00 -0.10
94 6.0970 0.00 -0.19 0.00 0.07
95 6.0970 0.00 -0.39 0.00 -0.26
96 6.0971 0.00 -0.13 0.00 -0.39
97 8.8739 0.00 0.51 0.00 0.09
98 8.8739 0.00 0.18 0.00 -0.74
99 8.8740 0.00 -0.62 0.00 0.45
100 9.0489 0.00 -0.07 0.00 -0.05
101 9.0489 0.00 0.04 0.00 -0.11
102 9.0490 0.00 -0.21 0.00 -0.21
103 9.9936 0.00 0.02 0.00 0.00
104 9.9936 0.00 0.26 0.00 0.16
105 9.9936 0.00 -0.32 0.00 0.07
106 9.9937 0.00 0.04 0.00 0.00
107 10.0781 0.00 -0.01 0.00 -0.09
108 10.0781 0.00 -0.13 0.00 0.17
109 10.0781 0.00 0.04 0.00 0.19
110 10.0782 0.00 0.02 0.00 -0.09
111 11.1976 0.00 0.06 0.00 0.17
112 11.1977 0.00 -0.05 0.00 -0.01
113 11.1977 0.00 0.12 0.00 0.07
114 11.1977 0.00 0.31 0.00 -0.06
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.
555758 quality flag:3 Type: 3:2E 3:2E 3:2E axisobj 39.225 39.225 39.225 ecceobj 0.254 0.254 0.254 incobj 24.223 24.223 24.223 qmin 26.343 26.342 26.343 qmax 53.134 53.137 53.132 amean 39.454 39.454 39.454 amin 39.026 39.009 39.016 amax 39.982 39.986 39.979 emean 0.269 0.268 0.269 emin 0.177 0.177 0.177 emax 0.331 0.331 0.331 imean 24.021 24.025 24.022 imin 21.691 21.690 21.691 imax 26.875 26.877 26.873 excite_mean 0.490 0.490 0.490 fracstop 1.000 1.000 1.000 cjmean 2.774 2.774 2.774 libcent 0 181.6 181.5 181.6 libamp 0 84.2 84.4 84.0 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 87.0 87.0 87.0 kozaiamp 58.0 58.0 58.0