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: 612349 # Created Fri Apr 26 01:09:12 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 55 observations of 60 # Arc: 14.83y # First observation: 2002/04/08 # Last observation: 2017/02/05 # Chi-squared of fit: 83.41 DOF: 104 RMS: 0.22 # Min/Max residuals: -0.63 0.54 # Exact a, adot, b, bdot, g, gdot: 1.360927E-05 2.048234E-02 8.450134E-06 1.024958E-02 2.403546E-02 2.175217E-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 -2.910349 -144.637473 0.291040 -0.048829 -0.959377 2452372.765463 # Heliocentric elements and errors Epoch: 2452372.5000 = 2002/04/08 Mean Anomaly: 93.34009 +/- 0.000 Argument of Peri: 249.82532 +/- 0.000 Long of Asc Node: 220.62735 +/- 0.000 Inclination: 26.73056 +/- 0.000 Eccentricity: 0.09292260 +/- 0.0000 Semi-Major Axis: 41.97820252 +/- 0.0000 Time of Perihelion: 2426615.2271 +/- 0.0 Perihelion: 38.07747861 +/- 0.0000 Aphelion: 45.87892643 +/- 0.0000 Period (y) 271.9844 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -34.83634043 +/- 0.0000 Ecliptic Y -24.36143163 +/- 0.0000 Ecliptic Z -2.11208880 +/- 0.0000 Ecliptic XDOT 0.00109178 +/- 0.0000 Ecliptic YDOT -0.00208158 +/- 0.0000 Ecliptic ZDOT 0.00115365 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 42.56179013 +/- 0.0000 Geocenter to KBO 41.60516378 +/- 0.0000 # Hcoef: 6.26
The following table shows the complete astrometric record for 612349. 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 (612349) followed by the observatory code and reference code for the source of the astrometry.
2002 04 08.26472 14 08 14.34 -16 03 05.0 20.7R 612349 807 Cf5154 2002 04 09.21801 14 08 10.10 -16 02 38.3 612349 807 Cf5154 2002 04 09.28159 14 08 09.84 -16 02 36.7 612349 807 Cf5154 2002 04 09.39501 14 08 09.28 -16 02 33.6 612349 807 Cf5154 2002 06 06.33293 14 04 02.80 -15 34 22.7 612349 568 Cf8972 2002 06 06.33587 14 04 02.78 -15 34 22.6 612349 568 Cf8972 2002 06 06.34081 14 04 02.78 -15 34 22.4 612349 568 Cf8972 2002 06 06.34624 14 04 02.75 -15 34 22.4 612349 568 Cf8972 2002 06 06.34998 14 04 02.74 -15 34 22.2 612349 568 Cf8972 2002 06 06.35299 14 04 02.74 -15 34 22.1 612349 568 Cf8972 2002 06 06.35594 14 04 02.74 -15 34 22.0 612349 568 Cf8972 2002 06 06.36088 14 04 02.71 -15 34 21.8 612349 568 Cf8972 2002 06 06.36632 14 04 02.69 -15 34 21.7 612349 568 Cf8972 2002 06 06.37006 14 04 02.68 -15 34 21.7 612349 568 Cf8972 2002 06 07.35895 14 03 59.58 -15 33 56.4 612349 568 Cf8972 2002 06 07.36191 14 03 59.57 -15 33 56.3 612349 568 Cf8972 2002 06 07.36685 14 03 59.55 -15 33 56.0 612349 568 Cf8972 2002 06 07.37229 14 03 59.53 -15 33 56.1 612349 568 Cf8972 2002 06 07.37603 14 03 59.52 -15 33 55.8 612349 568 Cf8972 2002 06 11.19237 14 03 48.18 -15 32 21.7 22.0R 612349 688 Cf7381 2002 06 11.26906 14 03 47.94 -15 32 19.6 612349 688 Cf7381 2003 05 30.03531 14 09 51.86 -15 28 30.0 21.2R 612349 807 Ci2129 2003 05 30.12813 14 09 51.51 -15 28 27.3 612349 807 Ci2129 2003 05 31.08532 14 09 48.00 -15 28 01.6 612349 807 Ci2129 2004 04 22.38818 14 17 55.42 -15 36 30.5 612349 568 Ck9583 2004 04 22.45251 14 17 55.10 -15 36 28.8 612349 568 Ck9583 2004 05 20.18606 14 15 50.16 -15 23 00.0 22.4R 612349 688 Ck8098 2004 05 20.26698 14 15 49.84 -15 22 57.7 612349 688 Ck8098 2009 03 31.22063 14 45 59.60 -14 50 00.4 20.2R 612349 950 C~08wZ 2009 03 31.22811 14 45 59.58 -14 50 01.0 22.0V 612349 950 C~08wZ 2009 03 31.23522 14 45 59.59 -14 50 01.0 21.9V 612349 950 C~08wZ 2009 03 31.24229 14 45 59.63 -14 50 01.6 21.8V 612349 950 C~08wZ 2009 03 31.24980 14 45 59.60 -14 50 00.7 20.3R 612349 950 C~08wZ 2011 03 31.17361 14 56 20.46 -14 24 38.1 22.5R 612349 304 C~0VlV 2011 03 31.17787 14 56 20.45 -14 24 37.9 612349 304 C~0VlV 2011 03 31.26213 14 56 20.14 -14 24 36.1 612349 304 C~0VlV 2011 03 31.26639 14 56 20.12 -14 24 36.1 612349 304 C~0VlV 2011 03 31.32838 14 56 19.92 -14 24 34.8 612349 304 C~0VlV 2011 03 31.33265 14 56 19.89 -14 24 34.5 612349 304 C~0VlV 2013 04 13.50396 15 05 39.614 -13 52 04.43 22.6G 612349 F51 C~2kHc 2013 06 04.38414 15 01 49.456 -13 31 00.90 23.2G 612349 F51 C~2kHc 2014 02 28.58240 15 12 40.510 -13 53 18.92 23.3G 612349 F51 C~2kHc 2014 05 08.44209 15 08 54.813 -13 27 46.09 22.9G 612349 F51 C~2kHc 2014 05 22.43833 15 07 50.699 -13 22 09.60 22.8G 612349 F51 C~2kHc 2014 05 24.37705 15 07 42.014 -13 21 25.29 22.9G 612349 F51 C~2kHc 2014 06 03.43376 15 06 58.576 -13 17 48.20 22.7G 612349 F51 C~2kHc 2014 06 21.36725 15 05 51.587 -13 12 25.76 22.9G 612349 F51 C~2kHc 2014 07 28.29790 15 04 41.086 -13 07 09.81 23.1G 612349 F51 C~2kHc 2015 06 23.37916 15 10 47.714 -12 58 12.92 22.5G 612349 F51 C~2kHc 2016 03 04.60636 15 22 32.390 -13 23 21.29 22.9G 612349 F51 C~2kHc 2016 03 15.56284 15 22 15.188 -13 20 02.69 22.9G 612349 F51 C~2kHc 2016 04 01.55171 15 21 29.720 -13 13 58.15 23.0G 612349 F51 C~2kHc 2016 04 16.57258 15 20 34.227 -13 07 59.11 22.9G 612349 F51 C~2kHc 2016 07 08.33902 15 15 04.618 -12 41 16.17 22.9G 612349 F51 C~2kHc 2017 02 05.65450 15 27 21.182 -13 14 09.26 23.1G 612349 F51 C~2kHc 2017 03 23.61071 15 26 55.161 -13 02 32.35 23.1G 612349 F51 C~2kHc 2017 04 27.48479 15 24 49.406 -12 48 49.79 23.1G 612349 F51 C~2kHc 2021 07 09.208210 15 39 38.223 -11 26 49.73 23.1G 612349 G37 C~4unc 2021 07 09.242880 15 39 38.118 -11 26 49.66 612349 G37 C~4unc 2021 07 09.275550 15 39 37.999 -11 26 50.28 612349 G37 C~4unc
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 -0.15 0.00 -0.32
2 0.0026 0.00 -0.28 0.00 -0.05
3 0.0028 0.00 0.14 0.00 -0.22
4 0.0031 0.00 -0.56 0.00 -0.31
5 0.1617 0.00 -0.03 0.00 0.06
6 0.1617 0.00 -0.19 0.00 0.09
7 0.1617 0.00 0.05 0.00 0.16
8 0.1618 0.00 -0.13 0.00 0.02
9 0.1618 0.00 -0.10 0.00 0.13
10 0.1618 0.00 0.05 0.00 0.15
11 0.1618 0.00 0.19 0.00 0.17
12 0.1618 0.00 -0.02 0.00 0.25
13 0.1618 0.00 -0.05 0.00 0.21
14 0.1618 0.00 -0.02 0.00 0.11
15 0.1645 0.00 0.08 0.00 0.22
16 0.1645 0.00 0.07 0.00 0.24
17 0.1646 0.00 0.01 0.00 0.42
18 0.1646 0.00 -0.03 0.00 0.18
19 0.1646 0.00 -0.00 0.00 0.39
20 0.1750 0.00 0.54 0.00 0.03
21 0.1752 0.00 0.30 0.00 0.27
22 1.1411 0.00 -0.07 0.00 -0.63
23 1.1413 0.00 -0.07 0.00 -0.43
24 1.1439 0.00 -0.09 0.00 -0.47
25 2.0400 0.00 0.37 0.00 -0.36
26 2.0402 0.00 0.11 0.00 -0.52
27 2.1161 0.00 -0.14 0.00 -0.16
28 2.1164 0.00 0.22 0.00 -0.13
29 6.9787 0.00 ( 5.23) 0.00 ( -0.87)
30 6.9787 0.00 ( 5.36) 0.00 ( -1.64)
31 6.9787 0.00 ( 5.91) 0.00 ( -1.81)
32 6.9787 0.00 ( 6.91) 0.00 ( -2.58)
33 6.9787 0.00 ( 6.89) 0.00 ( -1.86)
34 8.9772 0.00 0.01 0.00 0.20
35 8.9772 0.00 0.09 0.00 0.30
36 8.9774 0.00 -0.01 0.00 0.16
37 8.9774 0.00 -0.08 0.00 0.06
38 8.9776 0.00 0.28 0.00 -0.08
39 8.9776 0.00 0.06 0.00 0.12
40 11.0150 0.00 0.02 0.00 -0.48
41 11.1571 0.00 -0.13 0.00 -0.07
42 11.8941 0.00 -0.11 0.00 0.01
43 12.0826 0.00 -0.16 0.00 -0.14
44 12.1209 0.00 0.04 0.00 0.10
45 12.1262 0.00 -0.04 0.00 0.14
46 12.1538 0.00 -0.12 0.00 -0.08
47 12.2029 0.00 -0.19 0.00 0.06
48 12.3040 0.00 0.19 0.00 0.18
49 13.2077 0.00 -0.06 0.00 0.11
50 13.9065 0.00 -0.00 0.00 0.08
51 13.9365 0.00 0.17 0.00 -0.06
52 13.9830 0.00 0.14 0.00 0.02
53 14.0241 0.00 -0.00 0.00 -0.25
54 14.2507 0.00 0.01 0.00 0.11
55 14.8320 0.00 -0.26 0.00 0.08
56 14.9578 0.00 -0.13 0.00 0.02
57 15.0533 0.00 -0.02 0.00 -0.02
58 19.2524 0.00 0.34 0.00 0.33
59 19.2525 0.00 0.17 0.00 0.20
60 19.2526 0.00 -0.30 0.00 -0.60
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.
612349 quality flag:3 Type: SCATEXTD SCATEXTD SCATEXTD axisobj 41.792 41.792 41.792 ecceobj 0.091 0.091 0.091 incobj 26.774 26.774 26.774 qmin 37.634 37.624 37.637 qmax 46.724 46.696 46.718 amean 42.048 42.049 42.049 amin 41.721 41.721 41.719 amax 42.403 42.404 42.400 emean 0.086 0.086 0.086 emin 0.072 0.072 0.072 emax 0.102 0.102 0.102 imean 27.573 27.573 27.573 imin 27.239 27.239 27.239 imax 27.948 27.929 27.934 excite_mean 0.471 0.471 0.471 fracstop 1.000 1.000 1.000 cjmean 2.804 2.804 2.804 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 183.9 184.0 183.8 kozaiamp 180.0 180.0 179.9