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: 04OL14
# Created Sun Dec 22 02:08:41 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 14 observations of 14
# Arc: 11.13y
# First observation: 2004/07/17
# Last observation: 2015/09/05
# Chi-squared of fit: 9.73 DOF: 22 RMS: 0.15
# Min/Max residuals: -0.29 0.37
# Exact a, adot, b, bdot, g, gdot:
1.821976E-05 3.479565E-02 -6.174737E-06 -1.345803E-02 3.032564E-02 -1.131179E-03
# Covariance matrix:
4.7146E-13 -3.6222E-13 -6.6916E-14 1.5220E-13 5.2890E-13 -9.4351E-13
-3.6222E-13 6.2544E-13 1.1605E-13 -2.5921E-13 -2.0493E-13 1.5917E-12
-6.6916E-14 1.1605E-13 1.6961E-13 -6.3613E-14 -4.4682E-14 2.9849E-13
1.5220E-13 -2.5921E-13 -6.3613E-14 1.1360E-13 1.0857E-13 -6.6784E-13
5.2890E-13 -2.0493E-13 -4.4682E-14 1.0857E-13 1.3945E-12 -6.9521E-13
-9.4351E-13 1.5917E-12 2.9849E-13 -6.6784E-13 -6.9521E-13 4.1044E-12
# lat0 lon0 xBary yBary zBary JD0
1.953731 -61.391270 0.063627 0.034774 -1.016895 2453203.667513
# Heliocentric elements and errors
Epoch: 2453204.5000 = 2004/07/18
Mean Anomaly: 356.16645 +/- 0.008
Argument of Peri: 182.25863 +/- 0.016
Long of Asc Node: 123.37648 +/- 0.000
Inclination: 21.25815 +/- 0.000
Eccentricity: 0.30178299 +/- 0.0002
Semi-Major Axis: 48.58354630 +/- 0.0137
Time of Perihelion: 2454521.6380 +/- 51.8
Perihelion: 33.92185825 +/- 0.0126
Aphelion: 63.24523434 +/- 0.0196
Period (y) 338.6429 +/- 0.14
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X 16.20809999 +/- 0.0006
Ecliptic Y -29.85455460 +/- 0.0011
Ecliptic Z 1.12400930 +/- 0.0000
Ecliptic XDOT 0.00272668 +/- 0.0000
Ecliptic YDOT 0.00155044 +/- 0.0000
Ecliptic ZDOT -0.00121768 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 33.98914013 +/- 0.0010
Geocenter to KBO 32.97545054 +/- 0.0013
# Hcoef: 8.29
The following table shows the complete astrometric record for 04OL14. 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 (04OL14) followed by the observatory code and reference code for the source of the astrometry.
2004 07 17.16677 20 01 14.75 -18 31 32.6 22.5R 04OL14 807 Cl4371 2004 07 17.24396 20 01 14.29 -18 31 34.3 04OL14 807 Cl4371 2004 08 12.08663 19 58 47.51 -18 42 13.4 22.9R 04OL14 807 Cl4371 2004 08 12.19251 19 58 46.96 -18 42 16.1 04OL14 807 Cl4371 2004 09 11.03281 19 56 39.12 -18 53 09.3 23.6R 04OL14 304 Cl4371 2004 09 11.05975 19 56 39.04 -18 53 10.0 04OL14 304 Cl4371 2005 07 11.34052 20 10 44.24 -18 49 31.8 23.4R 04OL14 304 Co3996 2005 07 11.39366 20 10 43.91 -18 49 33.2 04OL14 304 Co3996 2005 08 08.07498 20 08 04.61 -19 01 24.1 22.8R 04OL14 807 Co3996 2005 08 08.19166 20 08 03.95 -19 01 26.8 04OL14 807 Co3996 2005 08 09.08009 20 07 59.05 -19 01 49.5 04OL14 807 Co3996 2015 09 05.03634 21 36 13.56 -21 11 54.6 24.7V 04OL14 W84 C~7mnz 2015 09 05.11164 21 36 13.17 -21 11 56.6 04OL14 W84 C~7mnz 2015 09 05.18721 21 36 12.77 -21 11 58.7 04OL14 W84 C~7mnz
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 0.02 0.00 -0.17
2 0.0002 0.00 -0.02 0.00 0.02
3 0.0710 0.00 -0.29 0.00 -0.09
4 0.0713 0.00 0.03 0.00 -0.23
5 0.1530 0.00 0.10 0.00 0.31
6 0.1530 0.00 0.17 0.00 0.12
7 0.9834 0.00 0.37 0.00 -0.03
8 0.9835 0.00 0.00 0.00 -0.11
9 1.0593 0.00 -0.14 0.00 -0.05
10 1.0596 0.00 -0.15 0.00 0.22
11 1.0620 0.00 -0.03 0.00 0.03
12 11.1345 0.00 -0.08 0.00 -0.05
13 11.1347 0.00 0.05 0.00 0.04
14 11.1349 0.00 0.05 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.
04OL14 quality flag:3 Type: SCATNEAR SCATNEAR SCATNEAR axisobj 48.738 48.738 48.739 ecceobj 0.305 0.305 0.305 incobj 21.228 21.228 21.228 qmin 32.057 32.429 31.653 qmax 67.634 66.840 69.836 amean 49.318 48.875 49.777 amin 48.215 47.775 48.285 amax 50.420 50.176 51.260 emean 0.321 0.314 0.336 emin 0.291 0.288 0.297 emax 0.351 0.339 0.370 imean 19.114 19.062 18.347 imin 18.021 18.009 16.826 imax 20.215 20.145 19.778 excite_mean 0.458 0.453 0.461 fracstop 1.000 1.000 1.000 cjmean 2.902 2.902 2.903 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 185.2 185.0 180.5 kozaiamp 180.0 180.0 180.0