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: 13CY133 # Created Sat Apr 20 01:14:17 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 96 observations of 96 # Arc: 6.36y # First observation: 2012/02/03 # Last observation: 2018/06/15 # Chi-squared of fit: 102.78 DOF: 186 RMS: 0.18 # Min/Max residuals: -0.82 0.62 # Exact a, adot, b, bdot, g, gdot: 3.776451E-05 4.064638E-01 1.248939E-05 1.262339E-01 1.707980E-01 -9.559899E-02 # Covariance matrix: 6.3442E-11 2.6180E-07 2.3341E-11 9.6311E-08 2.7291E-12 7.3813E-08 2.6180E-07 1.1544E-03 9.6649E-08 4.2457E-04 1.1504E-08 3.2541E-04 2.3341E-11 9.6649E-08 8.8202E-12 3.5537E-08 1.0074E-12 2.7248E-08 9.6311E-08 4.2457E-04 3.5537E-08 1.5638E-04 4.2317E-09 1.1970E-04 2.7291E-12 1.1504E-08 1.0074E-12 4.2317E-09 1.1837E-13 3.2432E-09 7.3813E-08 3.2541E-04 2.7248E-08 1.1970E-04 3.2432E-09 9.1746E-05 # lat0 lon0 xBary yBary zBary JD0 -3.980257 138.252366 0.071224 -0.068300 -0.981761 2455961.036396 # Heliocentric elements and errors Epoch: 2455960.5000 = 2012/02/03 Mean Anomaly: 312.78556 +/- 0.000 Argument of Peri: 62.61149 +/- 0.000 Long of Asc Node: 148.37971 +/- 0.000 Inclination: 17.70493 +/- 0.000 Eccentricity: 0.25819640 +/- 0.0019 Semi-Major Axis: 7.84931702 +/- 0.0000 Time of Perihelion: 2457013.9612 +/- 0.0 Perihelion: 5.82265162 +/- 0.0146 Aphelion: 9.87598242 +/- 0.0146 Period (y) 21.9916 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -5.04157249 +/- 0.0000 Ecliptic Y 4.59881285 +/- 0.0000 Ecliptic Z -0.40633743 +/- 0.0000 Ecliptic XDOT -0.00330714 +/- 0.0000 Ecliptic YDOT -0.00578115 +/- 0.0000 Ecliptic ZDOT 0.00212508 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 6.83610673 +/- 0.0000 Geocenter to KBO 5.85495511 +/- 0.0000 # Hcoef: 13.90
The following table shows the complete astrometric record for 13CY133. 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 (13CY133) followed by the observatory code and reference code for the source of the astrometry.
2012 02 03.53563 09 17 45.444 +11 34 06.00 21.9G 13CY133 F51 C~2kOm 2012 02 03.54852 09 17 45.148 +11 34 08.37 22.6G 13CY133 F51 C~2kOm 2012 02 03.56311 09 17 44.798 +11 34 10.98 21.5G 13CY133 F51 C~2kOm 2012 02 03.58203 09 17 44.347 +11 34 14.36 21.6G 13CY133 F51 C~2kOm 2012 02 04.50959 09 17 22.609 +11 37 02.73 21.9G 13CY133 F51 C~2kOm 2012 02 22.44448 09 10 27.606 +12 32 25.30 22.0G 13CY133 F51 C~2kOm 2013 02 14.39536 11 02 40.476 +10 49 12.06 21.6w 13CY133 F51 C~0p7u 2013 02 14.40991 11 02 40.178 +10 49 15.43 21.4w 13CY133 F51 C~0p7u 2013 02 14.41193 11 02 40.134 +10 49 15.91 21.5w 13CY133 F51 C~0p7u 2013 02 14.42452 11 02 39.870 +10 49 18.86 21.5w 13CY133 F51 C~0p7u 2013 02 14.42654 11 02 39.823 +10 49 19.35 21.5w 13CY133 F51 C~0p7u 2013 02 14.43924 11 02 39.566 +10 49 22.29 21.6w 13CY133 F51 C~0p7u 2013 02 14.44129 11 02 39.522 +10 49 22.79 21.4w 13CY133 F51 C~0p7u 2013 02 16.46851 11 01 57.73 +10 57 18.5 21.4R 13CY133 291 C~0p7u 2013 02 16.47974 11 01 57.45 +10 57 20.7 21.3R 13CY133 291 C~0p7u 2013 02 18.33951 11 01 18.31 +11 04 40.1 13CY133 291 C~0p7u 2013 02 18.36713 11 01 17.69 +11 04 46.7 20.9R 13CY133 291 C~0p7u 2013 02 18.52429 11 01 14.39 +11 05 24.8 20.1R 13CY133 E10 C~0p7u 2013 02 18.54503 11 01 13.93 +11 05 30.5 20.4R 13CY133 E10 C~0p7u 2013 03 03.44905 10 56 25.09 +11 56 19.5 20.7R 13CY133 291 C~0pTL 2013 03 03.47638 10 56 24.45 +11 56 26.3 13CY133 291 C~0pTL 2013 03 03.51128 10 56 23.671 +11 56 34.23 21.9G 13CY133 F51 C~2kOm 2013 03 14.31430 10 52 18.01 +12 36 59.8 21.1R 13CY133 695 C~0wCa 2013 03 14.42440 10 52 15.51 +12 37 23.4 13CY133 695 C~0wCa 2013 03 18.19400 10 50 53.44 +12 50 32.0 20.8R 13CY133 291 C~0qCH 2013 03 18.21562 10 50 52.95 +12 50 36.8 20.6R 13CY133 291 C~0qCH 2013 12 05.62468 12 46 59.535 +04 45 44.51 22.9G 13CY133 F51 C~2kOm 2013 12 05.62862 12 46 59.679 +04 45 44.26 22.9G 13CY133 F51 C~2kOm 2013 12 05.63257 12 46 59.791 +04 45 44.07 22.3G 13CY133 F51 C~2kOm 2013 12 05.63652 12 46 59.938 +04 45 43.72 22.3G 13CY133 F51 C~2kOm 2014 02 26.56984 13 04 01.971 +07 13 14.30 22.0G 13CY133 F51 C~2kOm 2014 02 26.58206 13 04 01.811 +07 13 17.44 21.9G 13CY133 F51 C~2kOm 2014 02 27.49330 13 03 50.614 +07 17 07.36 21.5w 13CY133 F51 C~240M 2014 02 27.50557 13 03 50.452 +07 17 10.51 21.7w 13CY133 F51 C~240M 2014 02 27.51785 13 03 50.295 +07 17 13.55 21.6w 13CY133 F51 C~240M 2014 03 09.48652 13 01 20.198 +08 00 05.47 21.7G 13CY133 F51 C~2kOm 2014 03 09.57366 13 01 18.643 +08 00 28.00 21.9G 13CY133 F51 C~2kOm 2014 03 09.59813 13 01 18.189 +08 00 34.19 21.2G 13CY133 F51 C~2kOm 2014 04 06.32417 12 51 32.54 +09 52 55.8 21.0V 13CY133 G96 C~240M 2014 04 06.33106 12 51 32.34 +09 52 58.1 21.8V 13CY133 G96 C~240M 2014 04 06.33796 12 51 32.20 +09 52 59.4 21.4V 13CY133 G96 C~240M 2014 04 06.34486 12 51 32.02 +09 53 00.8 21.4V 13CY133 G96 C~240M 2014 05 19.32860 12 39 06.854 +11 10 01.48 21.8G 13CY133 F51 C~2kOm 2014 05 19.34047 12 39 06.756 +11 10 01.41 21.8G 13CY133 F51 C~2kOm 2014 05 19.35250 12 39 06.642 +11 10 01.35 21.6G 13CY133 F51 C~2kOm 2014 05 19.36455 12 39 06.544 +11 10 01.19 21.7G 13CY133 F51 C~2kOm 2014 05 29.35713 12 38 14.673 +11 05 08.43 21.8G 13CY133 F51 C~2kOm 2014 06 28.18525 12 41 30.25 +10 06 15.5 22.0R 13CY133 G37 C~240M 2014 06 28.24809 12 41 31.18 +10 06 04.8 13CY133 G37 C~240M 2015 03 25.53728 15 08 32.529 +02 19 56.07 21.5w 13CY133 F51 C~240M 2015 03 25.54971 15 08 32.400 +02 19 58.86 21.6w 13CY133 F51 C~240M 2015 03 25.56216 15 08 32.244 +02 20 01.74 21.5w 13CY133 F51 C~240M 2015 03 27.52624 15 08 10.966 +02 27 25.91 21.7G 13CY133 F51 C~2kOm 2015 03 27.55052 15 08 10.671 +02 27 31.49 21.0G 13CY133 F51 C~2kOm 2015 03 27.56270 15 08 10.521 +02 27 34.12 20.5G 13CY133 F51 C~2kOm 2015 04 04.46407 15 06 23.227 +02 57 08.21 21.4G 13CY133 F51 C~2kOm 2015 04 04.47603 15 06 23.045 +02 57 10.78 21.4G 13CY133 F51 C~2kOm 2015 04 04.48802 15 06 22.849 +02 57 13.40 21.4G 13CY133 F51 C~2kOm 2015 04 12.39651 15 04 04.681 +03 25 41.37 21.6G 13CY133 F51 C~2kOm 2015 04 12.40886 15 04 04.446 +03 25 43.80 21.3G 13CY133 F51 C~2kOm 2015 04 12.46040 15 04 03.438 +03 25 54.69 21.7G 13CY133 F51 C~2kOm 2015 04 23.50170 15 00 10.545 +04 01 50.37 21.5G 13CY133 F51 C~2kOm 2015 04 23.53012 15 00 09.896 +04 01 55.45 21.5G 13CY133 F51 C~2kOm 2015 04 23.54437 15 00 09.558 +04 01 58.02 21.5G 13CY133 F51 C~2kOm 2015 04 24.31670 14 59 52.09 +04 04 14.8 21.3R 13CY133 G37 C~240M 2015 04 24.42765 14 59 49.49 +04 04 34.4 13CY133 G37 C~240M 2015 04 24.53427 14 59 47.030 +04 04 53.25 21.0G 13CY133 F51 C~2kOm 2015 04 24.56264 14 59 46.368 +04 04 58.33 21.1G 13CY133 F51 C~2kOm 2015 05 15.43059 14 51 31.238 +04 51 09.27 21.4G 13CY133 F51 C~2kOm 2015 05 15.44266 14 51 30.943 +04 51 10.06 21.1G 13CY133 F51 C~2kOm 2015 05 15.45475 14 51 30.656 +04 51 11.28 20.8G 13CY133 F51 C~2kOm 2015 05 15.46695 14 51 30.365 +04 51 12.62 21.5G 13CY133 F51 C~2kOm 2015 05 18.42985 14 50 21.859 +04 55 01.17 21.9w 13CY133 F51 C~240M 2015 05 18.44210 14 50 21.594 +04 55 01.80 21.5w 13CY133 F51 C~240M 2015 05 18.46669 14 50 21.004 +04 55 03.64 21.9w 13CY133 F51 C~240M 2015 06 22.34084 14 40 42.641 +04 42 45.60 21.9G 13CY133 F51 C~2kOm 2016 03 09.60767 17 03 59.687 -04 42 47.82 23.0G 13CY133 F51 C~2kOm 2016 03 18.61192 17 06 00.488 -04 21 02.27 22.5G 13CY133 F51 C~2kOm 2016 03 18.61922 17 06 00.553 -04 21 01.08 22.7G 13CY133 F51 C~2kOm 2016 03 18.62605 17 06 00.632 -04 20 59.89 22.2G 13CY133 F51 C~2kOm 2016 03 18.63285 17 06 00.693 -04 20 59.05 22.3G 13CY133 F51 C~2kOm 2016 05 15.52401 16 58 55.985 -02 05 06.93 21.8G 13CY133 F51 C~2kOm 2016 06 05.36824 16 50 35.148 -01 47 06.30 21.6w 13CY133 F51 C~240M 2016 06 05.37889 16 50 34.865 -01 47 05.96 21.8w 13CY133 F51 C~240M 2016 06 05.38951 16 50 34.608 -01 47 06.04 21.7w 13CY133 F51 C~240M 2016 06 05.40011 16 50 34.298 -01 47 06.15 21.7w 13CY133 F51 C~240M 2016 06 07.45203 16 49 43.185 -01 46 50.71 21.8G 13CY133 F51 C~2kOm 2016 06 07.47423 16 49 42.633 -01 46 50.44 21.6G 13CY133 F51 C~2kOm 2016 06 07.48540 16 49 42.352 -01 46 50.38 22.2G 13CY133 F51 C~2kOm 2016 06 29.37718 16 41 21.690 -02 01 53.63 21.6G 13CY133 F51 C~2kOm 2016 07 06.38253 16 39 13.150 -02 13 16.89 22.6G 13CY133 F51 C~2kOm 2016 07 31.27295 16 34 56.094 -03 14 47.52 22.0G 13CY133 F51 C~2kOm 2016 07 31.28490 16 34 56.040 -03 14 49.19 22.5G 13CY133 F51 C~2kOm 2016 07 31.29688 16 34 55.991 -03 14 51.36 22.4G 13CY133 F51 C~2kOm 2018 06 15.53353 20 11 48.394 -09 23 43.03 22.4w 13CY133 F51 C~2g3r 2018 06 15.54328 20 11 48.229 -09 23 43.70 22.3w 13CY133 F51 C~2g3r
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 -0.08 0.00 -0.15
2 0.0000 0.00 0.11 0.00 -0.09
3 0.0001 0.00 0.10 0.00 -0.10
4 0.0001 0.00 0.11 0.00 -0.12
5 0.0027 0.00 0.09 0.00 0.27
6 0.0518 0.00 0.07 0.00 0.01
7 1.0318 0.00 -0.15 0.00 0.13
8 1.0318 0.00 -0.07 0.00 0.08
9 1.0318 0.00 -0.10 0.00 0.09
10 1.0319 0.00 -0.11 0.00 0.08
11 1.0319 0.00 -0.19 0.00 0.10
12 1.0319 0.00 -0.06 0.00 0.06
13 1.0319 0.00 -0.07 0.00 0.08
14 1.0375 0.00 0.46 0.00 0.36
15 1.0375 0.00 -0.15 0.00 -0.07
16 1.0426 0.00 0.02 0.00 0.13
17 1.0427 0.00 -0.20 0.00 0.20
18 1.0431 0.00 -0.40 0.00 -0.54
19 1.0431 0.00 -0.50 0.00 0.23
20 1.0785 0.00 0.29 0.00 0.12
21 1.0786 0.00 0.26 0.00 0.60
22 1.0786 0.00 0.05 0.00 -0.01
23 1.1082 0.00 -0.08 0.00 -0.21
24 1.1085 0.00 -0.11 0.00 -0.07
25 1.1188 0.00 0.08 0.00 -0.27
26 1.1189 0.00 -0.15 0.00 0.10
27 1.8373 0.00 -0.06 0.00 -0.08
28 1.8374 0.00 0.13 0.00 -0.08
29 1.8374 0.00 -0.17 0.00 -0.02
30 1.8374 0.00 0.07 0.00 -0.12
31 2.0644 0.00 0.08 0.00 -0.01
32 2.0645 0.00 0.02 0.00 0.05
33 2.0670 0.00 0.09 0.00 -0.04
34 2.0670 0.00 0.10 0.00 0.00
35 2.0670 0.00 0.19 0.00 -0.07
36 2.0943 0.00 -0.08 0.00 0.20
37 2.0946 0.00 0.12 0.00 0.04
38 2.0946 0.00 -0.09 0.00 -0.13
39 2.1705 0.00 0.62 0.00 -0.82
40 2.1706 0.00 0.04 0.00 0.05
41 2.1706 0.00 0.37 0.00 -0.09
42 2.1706 0.00 0.10 0.00 -0.12
43 2.2883 0.00 -0.05 0.00 -0.02
44 2.2883 0.00 0.03 0.00 -0.05
45 2.2883 0.00 -0.11 0.00 -0.05
46 2.2884 0.00 -0.01 0.00 -0.16
47 2.3157 0.00 -0.10 0.00 0.10
48 2.3974 0.00 0.12 0.00 -0.01
49 2.3976 0.00 0.08 0.00 0.35
50 3.1376 0.00 0.04 0.00 -0.02
51 3.1376 0.00 0.14 0.00 -0.05
52 3.1376 0.00 -0.15 0.00 0.02
53 3.1430 0.00 -0.06 0.00 -0.30
54 3.1431 0.00 -0.08 0.00 -0.22
55 3.1431 0.00 -0.12 0.00 -0.34
56 3.1648 0.00 -0.24 0.00 0.07
57 3.1648 0.00 -0.04 0.00 -0.01
58 3.1648 0.00 -0.05 0.00 -0.05
59 3.1865 0.00 -0.39 0.00 0.09
60 3.1865 0.00 -0.26 0.00 -0.07
61 3.1867 0.00 -0.05 0.00 0.03
62 3.2169 0.00 -0.12 0.00 0.00
63 3.2170 0.00 0.09 0.00 0.00
64 3.2170 0.00 -0.00 0.00 0.03
65 3.2191 0.00 0.33 0.00 0.10
66 3.2194 0.00 0.32 0.00 0.18
67 3.2197 0.00 -0.11 0.00 -0.10
68 3.2198 0.00 -0.05 0.00 0.01
69 3.2769 0.00 -0.09 0.00 0.00
70 3.2770 0.00 -0.15 0.00 -0.23
71 3.2770 0.00 -0.09 0.00 -0.03
72 3.2770 0.00 -0.06 0.00 0.28
73 3.2851 0.00 -0.19 0.00 0.42
74 3.2852 0.00 0.16 0.00 0.20
75 3.2852 0.00 -0.02 0.00 0.34
76 3.3807 0.00 0.10 0.00 0.05
77 4.0960 0.00 0.14 0.00 -0.30
78 4.1207 0.00 0.02 0.00 -0.09
79 4.1207 0.00 -0.09 0.00 -0.00
80 4.1207 0.00 0.07 0.00 0.16
81 4.1207 0.00 -0.03 0.00 -0.02
82 4.2792 0.00 0.12 0.00 0.08
83 4.3363 0.00 0.15 0.00 0.13
84 4.3363 0.00 -0.01 0.00 0.34
85 4.3364 0.00 0.21 0.00 0.14
86 4.3364 0.00 -0.37 0.00 -0.10
87 4.3420 0.00 -0.12 0.00 -0.11
88 4.3421 0.00 0.08 0.00 0.08
89 4.3421 0.00 0.14 0.00 0.11
90 4.4020 0.00 -0.01 0.00 -0.00
91 4.4212 0.00 0.07 0.00 0.10
92 4.4894 0.00 0.07 0.00 -0.49
93 4.4894 0.00 -0.04 0.00 -0.00
94 4.4894 0.00 -0.08 0.00 -0.01
95 6.3628 0.00 0.08 0.00 0.20
96 6.3628 0.00 -0.11 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.
13CY133 quality flag:3 Type: CENTAURR CENTAURR CENTAURR axisobj 7.862 7.862 7.862 ecceobj 0.255 0.255 0.255 incobj 17.689 17.689 17.689 qmin 4.487 5.014 4.799 qmax 12.565 15.777 10.958 amean 8.198 8.810 7.595 amin 7.632 7.614 6.728 amax 8.671 10.396 8.194 emean 0.373 0.372 0.293 emin 0.255 0.255 0.255 emax 0.449 0.518 0.337 imean 16.086 16.753 15.664 imin 13.350 12.976 15.199 imax 17.687 18.220 16.525 excite_mean 0.467 0.475 0.400 fracstop 0.001 0.001 0.000 cjmean 4.604 4.403 4.912 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 86.2 127.0 85.0 kozaiamp 28.0 50.9 21.3