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: 03UT291 # Created Fri Nov 1 01:08:22 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 15 observations of 15 # Arc: 9.96y # First observation: 2003/10/22 # Last observation: 2013/10/07 # Chi-squared of fit: 18.81 DOF: 24 RMS: 0.20 # Min/Max residuals: -0.32 0.38 # Exact a, adot, b, bdot, g, gdot: 1.378259E-05 2.063120E-02 2.765931E-07 5.793167E-04 2.266349E-02 8.167468E-04 # Covariance matrix: 4.2515E-13 -2.2489E-13 4.0116E-15 -4.8621E-15 5.9155E-13 -8.0648E-13 -2.2489E-13 2.0546E-13 -4.2588E-15 5.1458E-15 -2.3423E-13 8.5071E-13 4.0116E-15 -4.2588E-15 1.6152E-13 -2.1605E-14 2.7445E-15 -1.8709E-14 -4.8621E-15 5.1458E-15 -2.1605E-14 7.3655E-15 -3.4117E-15 2.2588E-14 5.9155E-13 -2.3423E-13 2.7445E-15 -3.4117E-15 2.5190E-12 -5.8116E-13 -8.0648E-13 8.5071E-13 -1.8709E-14 2.2588E-14 -5.8116E-13 3.7310E-12 # lat0 lon0 xBary yBary zBary JD0 -0.106739 47.845973 0.334952 -0.001704 -0.938545 2452934.832203 # Heliocentric elements and errors Epoch: 2452934.5000 = 2003/10/22 Mean Anomaly: 149.26372 +/- 0.167 Argument of Peri: 203.72599 +/- 0.145 Long of Asc Node: 51.13694 +/- 0.001 Inclination: 1.61427 +/- 0.000 Eccentricity: 0.05997151 +/- 0.0002 Semi-Major Axis: 42.81937960 +/- 0.0117 Time of Perihelion: 2410500.8149 +/- 50.5 Perihelion: 40.25143690 +/- 0.0134 Aphelion: 45.38732230 +/- 0.0146 Period (y) 280.2004 +/- 0.12 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 30.48723178 +/- 0.0021 Ecliptic Y 33.18552371 +/- 0.0023 Ecliptic Z -0.08218351 +/- 0.0000 Ecliptic XDOT -0.00178611 +/- 0.0000 Ecliptic YDOT 0.00173988 +/- 0.0000 Ecliptic ZDOT 0.00006996 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 45.06390322 +/- 0.0022 Geocenter to KBO 44.12383954 +/- 0.0031 # Hcoef: 6.42
The following table shows the complete astrometric record for 03UT291. 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 (03UT291) followed by the observatory code and reference code for the source of the astrometry.
2003 10 22.33146 03 01 39.51 +17 02 54.3 22.6R 03UT291 695 Cj5825 2003 10 22.44609 03 01 39.00 +17 02 52.2 03UT291 695 Cj5825 2003 11 21.21853 02 59 22.48 +16 53 29.7 22.4R 03UT291 695 Cj5825 2003 11 21.29144 02 59 22.15 +16 53 27.9 03UT291 695 Cj5825 2004 10 10.37387 03 07 08.30 +17 27 27.2 22.4R 03UT291 695 Cl9848 2004 10 10.44355 03 07 08.03 +17 27 26.3 03UT291 695 Cl9848 2004 11 09.23799 03 04 57.24 +17 18 42.2 22.6R 03UT291 695 Cl9848 2004 11 09.33027 03 04 56.78 +17 18 40.5 03UT291 695 Cl9848 2004 11 10.31259 03 04 52.18 +17 18 21.9 03UT291 695 Cl9848 2006 10 21.365892 03 15 52.10 +18 06 08.5 22.9V 03UT291 645 C~2Jx9 2006 10 21.366721 03 15 52.09 +18 06 08.5 22.8V 03UT291 645 C~2Jx9 2006 10 21.369209 03 15 52.10 +18 06 08.7 23.2V 03UT291 645 C~2Jx9 2013 10 06.49297 03 50 15.63 +20 19 27.1 23.2R 03UT291 695 C~0zdX 2013 10 07.32029 03 50 13.06 +20 19 19.9 03UT291 695 C~0zdX 2013 10 07.40225 03 50 12.83 +20 19 19.2 03UT291 695 C~0zdX
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 0.12 0.00 0.06
2 0.0003 0.00 0.09 0.00 0.02
3 0.0818 0.00 0.05 0.00 0.32
4 0.0820 0.00 0.16 0.00 -0.11
5 0.9693 0.00 -0.23 0.00 0.15
6 0.9695 0.00 -0.17 0.00 0.33
7 1.0511 0.00 0.06 0.00 -0.08
8 1.0513 0.00 -0.26 0.00 -0.04
9 1.0540 0.00 -0.31 0.00 -0.12
10 2.9980 0.00 0.17 0.00 -0.32
11 2.9980 0.00 0.07 0.00 -0.31
12 2.9980 0.00 0.38 0.00 -0.07
13 9.9580 0.00 -0.06 0.00 -0.11
14 9.9603 0.00 -0.26 0.00 0.13
15 9.9605 0.00 0.23 0.00 0.17
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.
03UT291 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 43.143 43.143 43.143 ecceobj 0.056 0.056 0.056 incobj 1.607 1.607 1.607 qmin 39.662 39.662 39.652 qmax 46.271 46.261 46.269 amean 42.848 42.848 42.848 amin 42.519 42.518 42.520 amax 43.193 43.195 43.193 emean 0.051 0.051 0.051 emin 0.028 0.028 0.028 emax 0.071 0.071 0.072 imean 1.490 1.490 1.490 imin 0.000 0.000 0.000 imax 2.172 2.172 2.172 excite_mean 0.058 0.058 0.058 fracstop 1.000 1.000 1.000 cjmean 3.084 3.084 3.084 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 178.4 178.6 178.4 kozaiamp 180.0 179.9 180.0