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: 434390
# Created Sun Nov 24 02:07:02 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 37 observations of 37
# Arc: 17.16y
# First observation: 2005/02/10
# Last observation: 2022/04/08
# Chi-squared of fit: 71.37 DOF: 68 RMS: 0.25
# Min/Max residuals: -0.80 0.68
# Exact a, adot, b, bdot, g, gdot:
1.724990E-05 3.201358E-02 1.524515E-06 2.788188E-03 2.729798E-02 -1.674135E-04
# 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
1.319426 137.128075 -0.073907 0.022697 -0.980498 2453411.809733
# Heliocentric elements and errors
Epoch: 2453412.5000 = 2005/02/11
Mean Anomaly: 359.47546 +/- 0.000
Argument of Peri: 15.60961 +/- 0.000
Long of Asc Node: 122.78425 +/- 0.000
Inclination: 5.13249 +/- 0.000
Eccentricity: 0.32495982 +/- 0.0000
Semi-Major Axis: 55.72234936 +/- 0.0000
Time of Perihelion: 2453633.8702 +/- 0.0
Perihelion: 37.61482453 +/- 0.0000
Aphelion: 73.82987420 +/- 0.0000
Period (y) 415.9607 +/- 0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -27.61395786 +/- 0.0000
Ecliptic Y 25.52956739 +/- 0.0000
Ecliptic Z 0.84356452 +/- 0.0000
Ecliptic XDOT -0.00216766 +/- 0.0000
Ecliptic YDOT -0.00237611 +/- 0.0000
Ecliptic ZDOT 0.00027925 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 37.61650330 +/- 0.0000
Geocenter to KBO 36.63278504 +/- 0.0000
# Hcoef: 8.12
The following table shows the complete astrometric record for 434390. 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 (434390) followed by the observatory code and reference code for the source of the astrometry.
2005 02 10.30899 09 19 58.88 +16 57 32.3 24.2g 434390 568 C~0X5e 2005 02 10.39196 09 19 58.44 +16 57 34.6 24.1g 434390 568 C~0X5e 2005 02 10.43152 09 19 58.22 +16 57 35.4 24.1g 434390 568 C~0X5e 2005 02 15.33214 09 19 32.58 +16 59 40.4 23.9g 434390 568 C~0X5e 2005 04 11.30482 09 16 05.72 +17 15 36.8 24.1i 434390 568 C~0X5e 2005 04 11.33442 09 16 05.68 +17 15 36.9 24.0i 434390 568 C~0X5e 2005 04 11.35929 09 16 05.63 +17 15 37.1 23.9i 434390 568 C~0X5e 2006 02 03.47735 09 28 06.21 +16 29 26.1 434390 568 C~0X5e 2006 02 06.32831 09 27 51.29 +16 30 42.8 434390 568 C~0X5e 2006 02 06.36907 09 27 51.08 +16 30 43.7 434390 568 C~0X5e 2006 02 06.40730 09 27 50.88 +16 30 44.7 23.8r 434390 568 C~0X5e 2006 03 02.22794 09 25 49.18 +16 40 47.3 24.0R 434390 695 C~0X5e 2006 03 02.28430 09 25 48.92 +16 40 48.5 434390 695 C~0X5e 2006 03 02.34040 09 25 48.65 +16 40 49.8 434390 695 C~0X5e 2007 02 14.46983 09 34 37.68 +16 08 17.4 434390 568 C~0X5e 2007 02 14.50376 09 34 37.50 +16 08 18.4 434390 568 C~0X5e 2007 02 14.53694 09 34 37.32 +16 08 19.3 434390 568 C~0X5e 2007 02 15.48068 09 34 32.42 +16 08 44.7 434390 568 C~0X5e 2010 03 19.15000 09 54 05.29 +14 59 35.3 434390 675 C~0X5e 2010 03 19.18255 09 54 05.16 +14 59 35.7 434390 675 C~0X5e 2010 03 20.14302 09 54 01.24 +14 59 55.9 434390 675 C~0X5e 2010 03 20.17381 09 54 01.10 +14 59 56.8 434390 675 C~0X5e 2015 02 18.27179 10 32 19.67 +12 13 34.7 23.3R 434390 695 C~1M6D 2015 02 18.36258 10 32 19.20 +12 13 37.7 434390 695 C~1M6D 2015 02 18.45491 10 32 18.74 +12 13 40.5 434390 695 C~1M6D 2015 03 23.14543 10 29 41.63 +12 29 12.1 23.2R 434390 695 C~1Q3K 2015 03 23.21118 10 29 41.33 +12 29 13.6 434390 695 C~1Q3K 2015 03 23.27204 10 29 41.07 +12 29 15.1 434390 695 C~1Q3K 2015 04 15.19178 10 28 17.54 +12 36 40.3 23.4R 434390 695 C~1RHV 2015 04 15.27027 10 28 17.29 +12 36 41.3 434390 695 C~1RHV 2015 04 15.34305 10 28 17.11 +12 36 42.8 434390 695 C~1RHV 2020 02 18.259920 11 06 46.244 +09 26 46.31 23.8G 434390 G37 C~3n4O 2020 02 18.351190 11 06 45.841 +09 26 49.24 434390 G37 C~3n4O 2020 02 18.402160 11 06 45.611 +09 26 50.68 434390 G37 C~3n4O 2022 04 08.139760 11 16 16.100 +08 42 31.27 23.7G 434390 G37 C~5aQQ 2022 04 08.174430 11 16 15.963 +08 42 32.10 434390 G37 C~5aQQ 2022 04 08.209560 11 16 15.817 +08 42 32.84 434390 G37 C~5aQQ
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 0.27 0.00 -0.06
2 0.0002 0.00 0.34 0.00 0.09
3 0.0003 0.00 0.22 0.00 -0.13
4 0.0138 0.00 0.63 0.00 0.32
5 0.1643 0.00 -0.15 0.00 0.12
6 0.1643 0.00 -0.02 0.00 0.02
7 0.1644 0.00 -0.15 0.00 0.07
8 0.9806 0.00 -0.15 0.00 0.08
9 0.9884 0.00 -0.08 0.00 0.68
10 0.9885 0.00 0.03 0.00 0.48
11 0.9886 0.00 0.09 0.00 0.45
12 1.0539 0.00 -0.27 0.00 -0.17
13 1.0540 0.00 -0.06 0.00 -0.27
14 1.0542 0.00 -0.03 0.00 -0.26
15 2.0100 0.00 -0.13 0.00 -0.30
16 2.0101 0.00 -0.13 0.00 -0.21
17 2.0102 0.00 -0.20 0.00 -0.20
18 2.0128 0.00 0.00 0.00 -0.10
19 5.1002 0.00 -0.80 0.00 0.05
20 5.1003 0.00 -0.67 0.00 -0.25
21 5.1029 0.00 0.27 0.00 -0.46
22 5.1030 0.00 0.11 0.00 -0.21
23 10.0204 0.00 0.19 0.00 -0.06
24 10.0207 0.00 -0.03 0.00 0.14
25 10.0209 0.00 0.01 0.00 0.11
26 10.1104 0.00 0.23 0.00 0.00
27 10.1106 0.00 0.09 0.00 -0.10
28 10.1108 0.00 0.23 0.00 -0.08
29 10.1735 0.00 0.14 0.00 -0.09
30 10.1737 0.00 -0.18 0.00 -0.18
31 10.1739 0.00 0.27 0.00 0.32
32 15.0197 0.00 -0.22 0.00 0.02
33 15.0200 0.00 0.11 0.00 0.07
34 15.0201 0.00 0.22 0.00 -0.10
35 17.1549 0.00 -0.10 0.00 0.10
36 17.1550 0.00 -0.04 0.00 0.13
37 17.1551 0.00 -0.08 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.
434390 quality flag:3 Type: SCATNEAR SCATNEAR SCATNEAR axisobj 55.287 55.287 55.287 ecceobj 0.319 0.319 0.319 incobj 5.139 5.139 5.139 qmin 36.750 36.682 36.610 qmax 74.599 74.576 74.694 amean 55.118 55.113 55.123 amin 54.473 54.478 54.474 amax 55.997 55.971 55.968 emean 0.318 0.318 0.318 emin 0.304 0.304 0.305 emax 0.333 0.334 0.335 imean 3.418 3.414 3.423 imin 2.813 2.861 2.798 imax 4.125 4.136 4.131 excite_mean 0.323 0.323 0.324 fracstop 1.000 1.000 1.000 cjmean 3.107 3.107 3.107 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 173.0 171.1 175.9 kozaiamp 180.0 179.9 180.0