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: 03UN292
# Created Sun Nov 24 02:08:29 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 16 observations of 16
# Arc: 12.28y
# First observation: 2003/10/24
# Last observation: 2016/02/04
# Chi-squared of fit: 30.37 DOF: 26 RMS: 0.24
# Min/Max residuals: -0.73 0.45
# Exact a, adot, b, bdot, g, gdot:
1.628094E-05 2.534345E-02 9.467149E-07 3.338628E-04 2.486515E-02 -1.479588E-03
# Covariance matrix:
3.0032E-13 -8.3590E-14 1.2572E-15 -1.2697E-15 3.7419E-13 -3.8215E-13
-8.3590E-14 5.9252E-14 -9.2586E-16 7.4089E-16 2.5042E-14 1.8343E-13
1.2572E-15 -9.2586E-16 1.6849E-13 -2.1452E-14 7.8636E-16 -3.6893E-15
-1.2697E-15 7.4089E-16 -2.1452E-14 5.8371E-15 -2.4151E-15 3.6995E-15
3.7419E-13 2.5042E-14 7.8636E-16 -2.4151E-15 2.7438E-12 -1.0572E-12
-3.8215E-13 1.8343E-13 -3.6893E-15 3.6995E-15 -1.0572E-12 1.1081E-12
# lat0 lon0 xBary yBary zBary JD0
0.462211 54.915660 0.415721 0.007348 -0.904869 2452936.878223
# Heliocentric elements and errors
Epoch: 2452936.5000 = 2003/10/24
Mean Anomaly: 324.86846 +/- 0.066
Argument of Peri: 74.05505 +/- 0.083
Long of Asc Node: 23.71845 +/- 0.007
Inclination: 0.88736 +/- 0.000
Eccentricity: 0.11189957 +/- 0.0001
Semi-Major Axis: 45.03066610 +/- 0.0134
Time of Perihelion: 2463707.4897 +/- 48.7
Perihelion: 39.99175405 +/- 0.0136
Aphelion: 50.06957815 +/- 0.0163
Period (y) 302.1835 +/- 0.13
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X 23.97184701 +/- 0.0015
Ecliptic Y 33.41389063 +/- 0.0022
Ecliptic Z 0.32447083 +/- 0.0000
Ecliptic XDOT -0.00238203 +/- 0.0000
Ecliptic YDOT 0.00146434 +/- 0.0000
Ecliptic ZDOT 0.00003561 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 41.12476865 +/- 0.0020
Geocenter to KBO 40.21699885 +/- 0.0027
# Hcoef: 7.43
The following table shows the complete astrometric record for 03UN292. 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 (03UN292) followed by the observatory code and reference code for the source of the astrometry.
2003 10 24.37748 03 29 46.71 +19 26 40.4 23.1R 03UN292 695 Cj5825 2003 10 24.47026 03 29 46.30 +19 26 39.0 03UN292 695 Cj5825 2003 11 20.27822 03 27 32.61 +19 18 51.9 22.9R 03UN292 695 Cj5825 2003 11 20.35000 03 27 32.24 +19 18 50.6 03UN292 695 Cj5825 2004 10 10.41338 03 36 40.89 +19 51 35.7 22.3R 03UN292 695 Cl9848 2004 10 10.48100 03 36 40.64 +19 51 34.5 03UN292 695 Cl9848 2004 11 09.37548 03 34 23.54 +19 44 02.4 22.6R 03UN292 695 Cl9848 2004 11 09.46925 03 34 23.08 +19 44 00.8 03UN292 695 Cl9848 2007 11 09.32991 03 52 39.37 +20 46 16.9 03UN292 695 Cy4001 2007 11 09.37446 03 52 39.14 +20 46 16.1 03UN292 695 Cy4001 2008 11 20.25721 03 57 48.02 +21 02 38.1 24.6R 03UN292 250 S~06Af 2008 11 20.26416 03 57 47.98 +21 02 38.0 03UN292 250 S~06Af 2008 11 20.27041 03 57 47.95 +21 02 37.8 03UN292 250 S~06Af 2008 11 20.27735 03 57 47.91 +21 02 37.8 03UN292 250 S~06Af 2016 02 04.16200 04 36 38.60 +22 44 01.9 23.7R 03UN292 G37 C~1lv5 2016 02 04.29312 04 36 38.33 +22 44 01.2 03UN292 G37 C~1lv5
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 0.00 0.00 -0.16
2 0.0003 0.00 0.37 0.00 -0.08
3 0.0737 0.00 -0.14 0.00 0.05
4 0.0738 0.00 -0.07 0.00 0.06
5 0.9638 0.00 -0.18 0.00 0.45
6 0.9640 0.00 0.01 0.00 0.08
7 1.0459 0.00 -0.19 0.00 -0.04
8 1.0461 0.00 0.20 0.00 -0.00
9 4.0437 0.00 -0.18 0.00 -0.60
10 4.0438 0.00 -0.17 0.00 -0.73
11 5.0756 0.00 0.13 0.00 0.28
12 5.0757 0.00 0.08 0.00 0.29
13 5.0757 0.00 0.12 0.00 0.18
14 5.0757 0.00 0.07 0.00 0.29
15 12.2814 0.00 0.13 0.00 0.04
16 12.2818 0.00 -0.16 0.00 -0.05
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.
03UN292 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 45.346 45.346 45.346 ecceobj 0.114 0.114 0.114 incobj 0.883 0.883 0.883 qmin 39.003 39.009 38.991 qmax 51.272 51.259 51.269 amean 44.985 44.985 44.985 amin 44.605 44.621 44.616 amax 45.396 45.384 45.387 emean 0.115 0.115 0.115 emin 0.100 0.099 0.100 emax 0.130 0.130 0.130 imean 1.545 1.545 1.545 imin 0.773 0.773 0.774 imax 2.154 2.154 2.154 excite_mean 0.118 0.118 0.118 fracstop 1.000 1.000 1.000 cjmean 3.096 3.096 3.096 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 171.4 171.3 171.3 kozaiamp 180.0 180.0 180.0