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: 613412
# Created Thu Apr 25 01:09:20 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 41 observations of 41
# Arc: 10.94y
# First observation: 2006/04/27
# Last observation: 2017/04/04
# Chi-squared of fit: 54.76 DOF: 76 RMS: 0.20
# Min/Max residuals: -0.55 0.61
# Exact a, adot, b, bdot, g, gdot:
1.636925E-05 2.324238E-02 -3.056465E-06 -6.676615E-03 2.274871E-02 -8.548982E-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
0.197206 -139.896302 0.058808 0.003558 -1.000283 2453852.737254
# Heliocentric elements and errors
Epoch: 2453852.5000 = 2006/04/27
Mean Anomaly: 343.78525 +/- 0.000
Argument of Peri: 236.75042 +/- 0.000
Long of Asc Node: 40.70141 +/- 0.000
Inclination: 16.00047 +/- 0.000
Eccentricity: 0.54225014 +/- 0.0000
Semi-Major Axis: 82.27283705 +/- 0.0000
Time of Perihelion: 2466129.4589 +/- 0.0
Perihelion: 37.66037981 +/- 0.0000
Aphelion: 126.88529429 +/- 0.0000
Period (y) 746.2647 +/- 0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -34.42881396 +/- 0.0000
Ecliptic Y -28.91956687 +/- 0.0000
Ecliptic Z 0.15116704 +/- 0.0000
Ecliptic XDOT 0.00259058 +/- 0.0000
Ecliptic YDOT -0.00148428 +/- 0.0000
Ecliptic ZDOT -0.00080711 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 44.96366215 +/- 0.0000
Geocenter to KBO 43.95882955 +/- 0.0000
# Hcoef: 7.00
The following table shows the complete astrometric record for 613412. 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 (613412) followed by the observatory code and reference code for the source of the astrometry.
2006 04 27.23650 14 31 01.72 -14 39 35.0 21.8R 613412 807 Cr3609 2006 04 27.38137 14 31 01.08 -14 39 32.5 613412 807 Cr3609 2006 04 28.16137 14 30 57.61 -14 39 18.5 613412 807 Cr3609 2006 06 19.99374 14 27 33.87 -14 26 26.3 23.0R 613412 304 Cr4858 2006 06 20.08726 14 27 33.62 -14 26 25.5 613412 304 Cr4858 2006 08 21.02251 14 27 23.55 -14 29 48.2 22.0R 613412 807 Cs2782 2006 08 22.02112 14 27 26.01 -14 30 04.1 613412 807 Cs2782 2006 08 23.02379 14 27 28.55 -14 30 20.2 613412 807 Cs2782 2007 06 16.00204 14 32 29.36 -15 14 11.9 613412 304 Cy6786 2007 06 16.07550 14 32 29.14 -15 14 11.0 613412 304 Cy6786 2007 07 15.02400 14 31 32.26 -15 11 26.4 613412 304 Cy6786 2007 07 16.05277 14 31 31.46 -15 11 26.1 613412 304 Cy6786 2008 05 03.30278 14 40 14.79 -16 12 31.7 613412 695 Cz0452 2008 05 03.34326 14 40 14.62 -16 12 31.0 613412 695 Cz0452 2012 05 14.40873 15 00 14.351 -19 23 14.06 22.8G 613412 F51 C~3442 2012 05 19.38645 14 59 50.761 -19 21 55.78 23.7G 613412 F51 C~3442 2012 05 20.37215 14 59 46.143 -19 21 40.12 23.6G 613412 F51 C~3442 2012 06 08.30901 14 58 23.231 -19 16 53.09 22.9G 613412 F51 C~3442 2013 06 01.35873 15 04 24.441 -20 07 43.66 23.2G 613412 F51 C~3442 2013 06 01.37354 15 04 24.378 -20 07 43.43 23.6G 613412 F51 C~3442 2013 06 01.38835 15 04 24.316 -20 07 42.89 23.0G 613412 F51 C~3442 2014 04 30.47476 15 12 40.088 -21 04 48.19 23.0G 613412 F51 C~3442 2014 05 08.46770 15 12 01.042 -21 02 57.85 22.4G 613412 F51 C~3442 2014 05 08.47979 15 12 00.986 -21 02 57.74 23.2G 613412 F51 C~3442 2014 05 08.49191 15 12 00.934 -21 02 57.91 23.2G 613412 F51 C~3442 2014 05 08.50402 15 12 00.874 -21 02 57.65 23.5G 613412 F51 C~3442 2014 05 20.37838 15 11 02.566 -21 00 02.19 23.7G 613412 F51 C~3442 2014 05 20.38970 15 11 02.518 -21 00 02.04 22.7G 613412 F51 C~3442 2014 05 20.40100 15 11 02.460 -21 00 01.66 24.0G 613412 F51 C~3442 2014 05 20.41229 15 11 02.395 -21 00 01.58 22.8G 613412 F51 C~3442 2014 07 01.31536 15 08 12.760 -20 50 28.29 23.4G 613412 F51 C~3442 2014 07 01.32665 15 08 12.763 -20 50 27.89 22.8G 613412 F51 C~3442 2014 07 01.34920 15 08 12.682 -20 50 27.41 22.9G 613412 F51 C~3442 2015 03 30.64199 15 20 43.791 -21 58 16.33 23.2G 613412 F51 C~3442 2015 05 20.10263 15 16 56.47 -21 49 24.5 613412 W84 C~1Tit 2015 05 21.10791 15 16 51.50 -21 49 09.8 24.1V 613412 W84 C~1Tit 2015 05 24.10031 15 16 36.80 -21 48 25.6 613412 W84 C~1Tit 2015 06 11.34848 15 15 12.689 -21 43 58.14 22.9G 613412 F51 C~3442 2016 03 07.61127 15 27 37.070 -22 46 10.53 22.4G 613412 F51 C~3442 2016 05 07.48265 15 23 57.678 -22 41 19.37 22.7G 613412 F51 C~3442 2017 04 04.51099 15 32 38.845 -23 34 38.89 22.8G 613412 F51 C~3442
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 -0.30
2 0.0004 0.00 0.06 0.00 -0.35
3 0.0025 0.00 -0.05 0.00 0.04
4 0.1472 0.00 -0.04 0.00 0.10
5 0.1474 0.00 -0.02 0.00 0.09
6 0.3170 0.00 -0.06 0.00 -0.10
7 0.3197 0.00 0.04 0.00 -0.06
8 0.3225 0.00 -0.01 0.00 0.23
9 1.1356 0.00 -0.11 0.00 0.11
10 1.1358 0.00 -0.01 0.00 0.24
11 1.2150 0.00 0.29 0.00 0.06
12 1.2178 0.00 0.46 0.00 0.21
13 2.0180 0.00 -0.44 0.00 -0.03
14 2.0181 0.00 -0.17 0.00 -0.02
15 6.0484 0.00 0.11 0.00 0.19
16 6.0620 0.00 0.11 0.00 -0.14
17 6.0647 0.00 0.15 0.00 -0.04
18 6.1166 0.00 0.25 0.00 0.52
19 7.0968 0.00 0.06 0.00 -0.26
20 7.0969 0.00 0.12 0.00 -0.25
21 7.0969 0.00 0.20 0.00 0.06
22 8.0089 0.00 0.02 0.00 -0.01
23 8.0307 0.00 -0.12 0.00 0.14
24 8.0308 0.00 -0.05 0.00 0.08
25 8.0308 0.00 0.08 0.00 -0.26
26 8.0308 0.00 0.09 0.00 -0.18
27 8.0634 0.00 -0.18 0.00 -0.29
28 8.0634 0.00 -0.06 0.00 -0.31
29 8.0634 0.00 -0.10 0.00 -0.10
30 8.0635 0.00 -0.23 0.00 -0.19
31 8.1782 0.00 -0.55 0.00 -0.19
32 8.1782 0.00 -0.02 0.00 0.10
33 8.1783 0.00 -0.25 0.00 0.34
34 8.9238 0.00 -0.03 0.00 0.25
35 9.0619 0.00 0.17 0.00 0.04
36 9.0647 0.00 0.18 0.00 -0.01
37 9.0729 0.00 0.15 0.00 0.01
38 9.1228 0.00 -0.20 0.00 -0.07
39 9.8628 0.00 -0.09 0.00 0.10
40 10.0294 0.00 0.19 0.00 -0.35
41 10.9385 0.00 0.16 0.00 0.61
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.
613412 quality flag:3 Type: SCATNEAR SCATNEAR SCATNEAR axisobj 80.249 80.248 80.250 ecceobj 0.533 0.533 0.533 incobj 16.087 16.087 16.087 qmin 36.737 36.741 36.655 qmax 128.384 128.550 128.593 amean 81.134 81.337 81.345 amin 79.844 79.965 80.020 amax 83.074 83.045 83.161 emean 0.534 0.535 0.534 emin 0.520 0.522 0.521 emax 0.547 0.548 0.548 imean 15.786 15.856 15.865 imin 15.073 15.125 15.101 imax 16.627 16.674 16.743 excite_mean 0.599 0.600 0.600 fracstop 1.000 1.000 1.000 cjmean 3.043 3.043 3.043 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 184.7 181.7 183.8 kozaiamp 179.9 180.0 179.9