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: 00QK226 # Created Fri Nov 1 01:08:02 2024 # Orbit generated from Bernstein formalism # Fitting 10 observations of 10 # Arc: 10.20d # First observation: 2000/08/25 # Last observation: 2000/09/04 # WARNING Fitting with energy constraint # WARNING and with gdot fixed = 0 # WARNING MRQMIN stopped after 13 iterations -- oscilliatory solution # Chi-squared of fit: 15.65 DOF: 16 RMS: 0.22 # Min/Max residuals: -0.41 0.51 # Exact a, adot, b, bdot, g, gdot: 1.180348E-05 2.087027E-02 -8.003145E-06 -1.446922E-02 2.596745E-02 0.000000E+00 # Covariance matrix: 6.8025E-11 1.1258E-07 -9.2814E-14 2.1700E-11 1.8115E-08 0.0000E+00 1.1258E-07 1.8775E-04 -1.5476E-10 3.6181E-08 3.0202E-05 0.0000E+00 -9.2814E-14 -1.5476E-10 4.8514E-13 -2.9860E-11 -2.4896E-11 0.0000E+00 2.1700E-11 3.6181E-08 -2.9860E-11 2.6386E-09 5.8203E-09 0.0000E+00 1.8115E-08 3.0202E-05 -2.4896E-11 5.8203E-09 4.8585E-06 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 2.3041E-04 # lat0 lon0 xBary yBary zBary JD0 -0.193630 -21.235940 0.120159 -0.003547 -1.000647 2451781.693023 # Heliocentric elements and errors Epoch: 2451780.5000 = 2000/08/24 Mean Anomaly: 188.11091 +/- 77.927 Argument of Peri: 352.85813 +/- 67.175 Long of Asc Node: 158.32612 +/- 0.192 Inclination: 34.70421 +/- 17.596 Eccentricity: 0.04172521 +/- 0.6072 Semi-Major Axis: 37.94557932 +/- 19.0105 Time of Perihelion: 2492545.3666 +/- 186738.5 Perihelion: 36.36229187 +/- 29.3724 Aphelion: 39.52886676 +/- 30.3819 Period (y) 233.7491 +/- 175.66 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 36.78958934 +/- 3.0468 Ecliptic Y -14.41821545 +/- 1.1843 Ecliptic Z -0.13046232 +/- 0.0111 Ecliptic XDOT 0.00078493 +/- 0.0016 Ecliptic YDOT 0.00205821 +/- 0.0013 Ecliptic ZDOT -0.00152539 +/- 0.0001 # Distances at JD0 (AU) Heliocenter to KBO 39.51424858 +/- 2.8694 Geocenter to KBO 38.50975666 +/- 3.2688 # Hcoef: 7.53
The following table shows the complete astrometric record for 00QK226. 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 (00QK226) followed by the observatory code and reference code for the source of the astrometry.
2000 08 25.19228 22 41 48.16 -08 27 48.4 24.3R 00QK226 807 Ch1309 2000 08 25.25424 22 41 47.86 -08 27 50.6 00QK226 807 Ch1309 2000 08 29.14079 22 41 29.39 -08 30 15.6 00QK226 809 Cb8401 2000 08 29.23793 22 41 28.94 -08 30 19.2 00QK226 809 Cb8401 2000 08 30.11911 22 41 24.76 -08 30 52.3 00QK226 809 Cb8401 2000 08 30.20674 22 41 24.32 -08 30 55.4 22.9R 00QK226 809 Cb8401 2000 08 30.28942 22 41 23.93 -08 30 58.2 00QK226 809 Cb8401 2000 08 30.33261 22 41 23.71 -08 30 59.8 00QK226 809 Cb8401 2000 08 30.38042 22 41 23.53 -08 31 01.6 00QK226 809 Cb8401 2000 09 04.394050 22 40 59.65 -08 34 09.3 22.1i 00QK226 645 C~5V7f
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 0.19 0.00 -0.17
2 0.0002 -4.95 0.20 -0.37 -0.06
3 0.0108 -313.34 -0.41 -32.11 0.07
4 0.0111 -320.88 -0.12 -32.95 -0.02
5 0.0135 -390.77 -0.12 -40.41 -0.22
6 0.0137 -397.99 -0.27 -40.84 0.03
7 0.0140 -404.40 -0.02 -41.27 0.24
8 0.0141 -408.02 -0.17 -41.53 0.31
9 0.0142 -411.17 0.51 -42.20 0.01
10 0.0279 -809.92 0.24 -83.59 -0.22
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.
00QK226 quality flag:0 Type: ERR2LARGE ERR2LARGE ERR2LARGE axisobj 0.000 0.000 0.000 ecceobj -1.000 -1.000 -1.000 incobj -1.000 -1.000 -1.000 qmin 0.000 0.000 0.000 qmax 0.000 0.000 0.000 amean 0.000 0.000 0.000 amin 0.000 0.000 0.000 amax 0.000 0.000 0.000 emean 0.000 0.000 0.000 emin 0.000 0.000 0.000 emax 0.000 0.000 0.000 imean 0.000 0.000 0.000 imin 0.000 0.000 0.000 imax 0.000 0.000 0.000 excite_mean 0.000 0.000 0.000 fracstop 0.000 0.000 0.000 cjmean 0.000 0.000 0.000 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 0.0 0.0 0.0 kozaiamp 0.0 0.0 0.0