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: 612175 # Created Fri Apr 26 01:09:09 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 74 observations of 74 # Arc: 21.04y # First observation: 2000/08/29 # Last observation: 2021/09/12 # Chi-squared of fit: 146.25 DOF: 142 RMS: 0.25 # Min/Max residuals: -1.60 0.53 # Exact a, adot, b, bdot, g, gdot: 1.550119E-05 1.973864E-02 4.205698E-07 -3.150106E-04 2.203336E-02 -1.201120E-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 -0.783341 -21.457842 0.047764 -0.013904 -1.005324 2451785.724523 # Heliocentric elements and errors Epoch: 2451786.5000 = 2000/08/30 Mean Anomaly: 235.65384 +/- 0.000 Argument of Peri: 351.74205 +/- 0.000 Long of Asc Node: 118.46672 +/- 0.000 Inclination: 1.19144 +/- 0.000 Eccentricity: 0.08258653 +/- 0.0000 Semi-Major Axis: 44.14635526 +/- 0.0000 Time of Perihelion: 2488792.3669 +/- 0.0 Perihelion: 40.50046105 +/- 0.0000 Aphelion: 47.79224946 +/- 0.0000 Period (y) 293.3259 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 43.16006593 +/- 0.0000 Ecliptic Y -17.00855277 +/- 0.0000 Ecliptic Z -0.62048709 +/- 0.0000 Ecliptic XDOT 0.00075055 +/- 0.0000 Ecliptic YDOT 0.00234278 +/- 0.0000 Ecliptic ZDOT -0.00003695 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 46.39473081 +/- 0.0000 Geocenter to KBO 45.38580132 +/- 0.0000 # Hcoef: 6.45
The following table shows the complete astrometric record for 612175. 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 (612175) followed by the observatory code and reference code for the source of the astrometry.
2000 08 29.22378 22 41 51.89 -09 05 36.0 612175 809 Cb8401 2000 08 30.10532 22 41 48.26 -09 05 57.9 612175 809 Cb8401 2000 08 30.19597 22 41 47.86 -09 06 00.3 612175 809 Cb8401 2000 08 30.27500 22 41 47.53 -09 06 02.0 22.5R 612175 809 Cb8401 2000 08 30.32187 22 41 47.33 -09 06 03.3 612175 809 Cb8401 2000 08 30.36952 22 41 47.14 -09 06 04.4 612175 809 Cb8401 2000 11 27.12435 22 38 06.01 -09 27 19.5 22.9R 612175 695 Cc3790 2000 11 28.15953 22 38 06.57 -09 27 13.1 22.4R 612175 695 Cc3790 2000 11 29.15392 22 38 07.21 -09 27 08.4 22.9R 612175 695 Cc3790 2005 08 08.11980 23 04 35.30 -06 51 58.2 21.7R 612175 807 Co3374 2005 08 08.23607 23 04 34.89 -06 52 01.0 612175 807 Co3374 2005 08 09.12496 23 04 31.76 -06 52 21.2 612175 807 Co3374 2006 08 22.26237 23 07 59.80 -06 31 52.9 21.7R 612175 807 Cs2440 2006 08 23.18631 23 07 56.18 -06 32 16.2 612175 807 Cs2440 2006 08 23.25480 23 07 55.90 -06 32 18.0 612175 807 Cs2440 2006 10 19.17414 23 04 17.94 -06 54 53.3 22.5R 612175 695 Ct0277 2006 10 19.26624 23 04 17.67 -06 54 54.9 612175 695 Ct0277 2006 10 20.16577 23 04 15.04 -06 55 10.5 612175 695 Ct0277 2006 12 21.09338 23 03 36.79 -06 58 06.0 22.4R 612175 695 Ct5425 2006 12 21.17556 23 03 36.92 -06 58 05.4 612175 695 Ct5425 2010 07 20.60742 23 26 51.614 -04 35 51.03 21.4G 612175 F51 C~343g 2010 09 16.30647 23 23 30.62 -04 57 57.4 22.6R 612175 688 C~0NFG 2010 09 16.35513 23 23 30.45 -04 57 58.9 612175 688 C~0NFG 2011 09 21.36646 23 27 30.410 -04 33 22.92 22.8G 612175 F51 C~343g 2011 09 21.39457 23 27 30.301 -04 33 23.44 22.9G 612175 F51 C~343g 2011 09 21.40862 23 27 30.236 -04 33 24.02 22.9G 612175 F51 C~343g 2012 10 06.35353 23 30 47.273 -04 13 14.12 22.5G 612175 F51 C~343g 2014 07 28.53911 23 43 44.564 -02 50 54.36 23.2G 612175 F51 C~343g 2014 07 28.55054 23 43 44.541 -02 50 54.51 22.1G 612175 F51 C~343g 2014 07 28.57331 23 43 44.484 -02 50 54.54 23.8G 612175 F51 C~343g 2014 08 05.52194 23 43 23.788 -02 53 18.88 23.9G 612175 F51 C~343g 2014 08 20.48120 23 42 35.572 -02 58 45.63 23.0G 612175 F51 C~343g 2014 08 22.47844 23 42 28.388 -02 59 33.67 22.5G 612175 F51 C~343g 2014 08 22.49068 23 42 28.327 -02 59 33.98 22.8G 612175 F51 C~343g 2014 08 22.50296 23 42 28.270 -02 59 34.06 22.7G 612175 F51 C~343g 2014 08 22.51523 23 42 28.233 -02 59 34.54 22.4G 612175 F51 C~343g 2014 09 17.36258 23 40 45.506 -03 10 51.01 22.9G 612175 F51 C~343g 2014 09 19.33339 23 40 37.324 -03 11 44.17 22.6G 612175 F51 C~343g 2014 09 19.36903 23 40 37.167 -03 11 45.46 23.0G 612175 F51 C~343g 2014 11 18.23718 23 37 23.789 -03 31 56.47 23.0G 612175 F51 C~343g 2014 11 26.28988 23 37 13.725 -03 32 51.16 23.7G 612175 F51 C~343g 2015 09 09.41754 23 45 39.709 -02 39 57.34 22.8G 612175 F51 C~343g 2015 09 09.42969 23 45 39.646 -02 39 57.79 22.7G 612175 F51 C~343g 2015 09 09.44186 23 45 39.599 -02 39 57.92 22.6G 612175 F51 C~343g 2015 09 10.39349 23 45 35.711 -02 40 23.71 22.6G 612175 F51 C~343g 2015 09 12.41868 23 45 27.386 -02 41 17.98 23.1G 612175 F51 C~343g 2015 09 12.43045 23 45 27.338 -02 41 18.37 23.1G 612175 F51 C~343g 2017 07 30.53307 23 56 36.302 -01 29 58.63 22.9G 612175 F51 C~343g 2017 08 01.53329 23 56 31.593 -01 30 31.58 22.9G 612175 F51 C~343g 2017 08 01.54515 23 56 31.556 -01 30 31.77 23.2G 612175 F51 C~343g 2017 08 01.55704 23 56 31.515 -01 30 31.81 22.3G 612175 F51 C~343g 2017 08 01.56895 23 56 31.494 -01 30 32.12 22.5G 612175 F51 C~343g 2017 08 03.52437 23 56 26.690 -01 31 05.65 22.6G 612175 F51 C~343g 2017 08 03.53513 23 56 26.646 -01 31 05.98 23.2G 612175 F51 C~343g 2017 08 03.54593 23 56 26.626 -01 31 06.55 22.5G 612175 F51 C~343g 2017 08 03.55668 23 56 26.586 -01 31 06.63 23.3G 612175 F51 C~343g 2017 08 20.57232 23 55 35.362 -01 36 58.18 23.5G 612175 F51 C~343g 2017 09 14.41468 23 53 59.622 -01 47 35.57 22.4G 612175 F51 C~343g 2017 09 17.42122 23 53 47.168 -01 48 57.49 22.8G 612175 F51 C~343g 2017 09 25.38210 23 53 14.051 -01 52 33.94 22.9G 612175 F51 C~343g 2017 09 25.40332 23 53 13.943 -01 52 34.25 22.5G 612175 F51 C~343g 2017 09 25.41391 23 53 13.879 -01 52 34.22 22.9G 612175 F51 C~343g 2017 09 26.38949 23 53 09.841 -01 53 00.87 22.3G 612175 F51 C~343g 2017 09 26.40129 23 53 09.782 -01 53 01.06 22.9G 612175 F51 C~343g 2017 09 26.41309 23 53 09.749 -01 53 01.19 22.5G 612175 F51 C~343g 2017 09 26.42490 23 53 09.692 -01 53 01.26 22.8G 612175 F51 C~343g 2017 09 28.43034 23 53 01.370 -01 53 55.45 23.6G 612175 F51 C~343g 2017 09 28.44211 23 53 01.347 -01 53 55.40 23.0G 612175 F51 C~343g 2017 09 28.45385 23 53 01.278 -01 53 55.85 22.7G 612175 F51 C~343g 2017 09 28.46562 23 53 01.260 -01 53 56.41 22.9G 612175 F51 C~343g 2017 11 13.28053 23 50 26.760 -02 10 08.66 23.7G 612175 F51 C~343g 2021 09 12.317360 00 11 44.783 +00 04 44.49 22.9G 612175 G37 C~552k 2021 09 12.377460 00 11 44.540 +00 04 42.98 612175 G37 C~552k 2021 09 12.437700 00 11 44.296 +00 04 41.30 612175 G37 C~552k
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 -0.21 0.00 -0.23
2 0.0024 0.00 0.02 0.00 -0.07
3 0.0027 0.00 -0.26 0.00 -0.19
4 0.0029 0.00 -0.21 0.00 0.08
5 0.0030 0.00 -0.25 0.00 -0.05
6 0.0031 0.00 -0.11 0.00 0.04
7 0.2461 0.00 0.49 0.00 -1.60
8 0.2490 0.00 0.33 0.00 0.43
9 0.2517 0.00 0.38 0.00 0.42
10 4.9415 0.00 0.08 0.00 0.21
11 4.9419 0.00 0.14 0.00 0.05
12 4.9443 0.00 0.08 0.00 0.06
13 5.9796 0.00 -0.10 0.00 0.07
14 5.9821 0.00 0.02 0.00 0.02
15 5.9823 0.00 -0.06 0.00 -0.05
16 6.1381 0.00 0.11 0.00 0.28
17 6.1384 0.00 0.22 0.00 0.31
18 6.1408 0.00 0.01 0.00 0.42
19 6.3104 0.00 0.06 0.00 0.38
20 6.3106 0.00 -0.27 0.00 -0.08
21 9.8902 0.00 -0.09 0.00 0.40
22 10.0481 0.00 -0.88 0.00 -0.39
23 10.0483 0.00 -0.37 0.00 -0.61
24 11.0613 0.00 0.08 0.00 -0.04
25 11.0614 0.00 0.21 0.00 0.18
26 11.0614 0.00 0.12 0.00 -0.03
27 12.1044 0.00 0.01 0.00 -0.17
28 13.9119 0.00 0.00 0.00 0.14
29 13.9119 0.00 0.07 0.00 0.18
30 13.9120 0.00 0.05 0.00 0.53
31 13.9337 0.00 0.36 0.00 -0.10
32 13.9747 0.00 0.02 0.00 -0.07
33 13.9802 0.00 0.24 0.00 0.09
34 13.9802 0.00 0.01 0.00 0.08
35 13.9802 0.00 -0.16 0.00 0.30
36 13.9803 0.00 -0.03 0.00 0.11
37 14.0510 0.00 0.11 0.00 0.25
38 14.0564 0.00 0.04 0.00 0.18
39 14.0565 0.00 -0.06 0.00 -0.15
40 14.2204 0.00 0.22 0.00 -0.01
41 14.2425 0.00 -0.15 0.00 0.06
42 15.0286 0.00 0.05 0.00 -0.03
43 15.0286 0.00 -0.14 0.00 -0.15
44 15.0287 0.00 -0.08 0.00 0.05
45 15.0313 0.00 -0.09 0.00 -0.18
46 15.0368 0.00 -0.12 0.00 0.12
47 15.0368 0.00 -0.10 0.00 0.05
48 16.9180 0.00 0.42 0.00 -0.26
49 16.9235 0.00 0.08 0.00 -0.12
50 16.9235 0.00 -0.03 0.00 -0.11
51 16.9236 0.00 -0.20 0.00 0.05
52 16.9236 0.00 -0.07 0.00 -0.06
53 16.9290 0.00 0.26 0.00 0.31
54 16.9290 0.00 0.02 0.00 0.17
55 16.9290 0.00 0.15 0.00 -0.20
56 16.9290 0.00 -0.03 0.00 -0.09
57 16.9756 0.00 -0.03 0.00 0.03
58 17.0436 0.00 0.08 0.00 0.17
59 17.0519 0.00 0.15 0.00 -0.07
60 17.0737 0.00 0.42 0.00 -0.49
61 17.0737 0.00 0.14 0.00 -0.23
62 17.0738 0.00 -0.15 0.00 0.08
63 17.0764 0.00 -0.03 0.00 -0.30
64 17.0765 0.00 -0.16 0.00 -0.17
65 17.0765 0.00 0.09 0.00 0.02
66 17.0765 0.00 -0.02 0.00 0.26
67 17.0820 0.00 -0.43 0.00 -0.19
68 17.0820 0.00 -0.03 0.00 0.17
69 17.0821 0.00 -0.33 0.00 0.04
70 17.0821 0.00 0.14 0.00 -0.21
71 17.2075 0.00 0.03 0.00 0.01
72 21.0379 0.00 -0.06 0.00 -0.06
73 21.0381 0.00 0.01 0.00 0.04
74 21.0382 0.00 0.06 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.
612175 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 44.231 44.231 44.231 ecceobj 0.081 0.081 0.081 incobj 1.191 1.191 1.191 qmin 39.245 39.252 39.235 qmax 49.170 49.191 49.206 amean 44.057 44.057 44.057 amin 43.696 43.690 43.705 amax 44.439 44.445 44.446 emean 0.090 0.090 0.090 emin 0.072 0.073 0.072 emax 0.107 0.107 0.107 imean 1.047 1.047 1.047 imin 0.063 0.063 0.063 imax 1.756 1.757 1.756 excite_mean 0.092 0.092 0.092 fracstop 1.000 1.000 1.000 cjmean 3.092 3.092 3.092 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 188.2 188.3 188.2 kozaiamp 180.0 180.0 180.0