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: 05PF23 # Created Wed Nov 27 02:08:46 2024 # Orbit generated from Bernstein formalism # Fitting 15 observations of 15 # Arc: 1.07d # First observation: 2005/08/02 # Last observation: 2005/08/03 # WARNING Fitting with energy constraint # WARNING and with gdot fixed = 0 # Chi-squared of fit: 9.04 DOF: 26 RMS: 0.14 # Min/Max residuals: -0.25 0.26 # Exact a, adot, b, bdot, g, gdot: 1.547269E-05 2.435935E-02 -8.915973E-08 -4.092974E-04 2.466200E-02 0.000000E+00 # Covariance matrix: 3.6490E-11 5.6457E-08 1.5224E-13 3.0693E-10 1.0387E-08 0.0000E+00 5.6457E-08 8.7833E-05 2.3654E-10 4.7688E-07 1.6138E-05 0.0000E+00 1.5224E-13 2.3654E-10 1.2758E-13 -3.8583E-11 4.3488E-11 0.0000E+00 3.0693E-10 4.7688E-07 -3.8583E-11 5.7339E-08 8.7677E-08 0.0000E+00 1.0387E-08 1.6138E-05 4.3488E-11 8.7677E-08 2.9671E-06 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 1.9738E-04 # lat0 lon0 xBary yBary zBary JD0 -0.561608 -20.307154 0.496475 -0.008605 -0.887116 2453585.019433 # Heliocentric elements and errors Epoch: 2453580.5000 = 2005/07/29 Mean Anomaly: 332.41026 +/- 351.380 Argument of Peri: 238.33311 +/- 54.468 Long of Asc Node: 129.47171 +/- 18.712 Inclination: 1.11483 +/- 0.643 Eccentricity: 0.02248606 +/- 0.5744 Semi-Major Axis: 42.27267185 +/- 21.8579 Time of Perihelion: 2461274.1628 +/- 399109.4 Perihelion: 41.32212582 +/- 32.3450 Aphelion: 43.22321788 +/- 33.0026 Period (y) 274.8513 +/- 213.18 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 38.68187013 +/- 2.6559 Ecliptic Y -14.84582638 +/- 0.9830 Ecliptic Z -0.39742223 +/- 0.0278 Ecliptic XDOT 0.00093962 +/- 0.0015 Ecliptic YDOT 0.00252947 +/- 0.0010 Ecliptic ZDOT -0.00004541 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 41.43481124 +/- 2.5043 Geocenter to KBO 40.54821502 +/- 2.8321 # Hcoef: 9.65
The following table shows the complete astrometric record for 05PF23. 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 (05PF23) followed by the observatory code and reference code for the source of the astrometry.
2005 08 02.51869 22 45 50.55 -08 27 18.7 05PF23 568 Cq7105 2005 08 02.52395 22 45 50.53 -08 27 19.0 05PF23 568 Cq7105 2005 08 02.52919 22 45 50.51 -08 27 18.7 25.5R 05PF23 568 Cq7106 2005 08 02.53442 22 45 50.50 -08 27 18.9 05PF23 568 Cq7106 2005 08 02.54495 22 45 50.44 -08 27 19.6 05PF23 568 Cq7106 2005 08 02.61299 22 45 50.18 -08 27 20.9 05PF23 568 Cq7106 2005 08 02.61821 22 45 50.14 -08 27 21.0 05PF23 568 Cq7106 2005 08 02.62343 22 45 50.13 -08 27 21.1 05PF23 568 Cq7106 2005 08 03.49521 22 45 46.77 -08 27 42.1 05PF23 568 Cq7106 2005 08 03.50044 22 45 46.76 -08 27 42.3 05PF23 568 Cq7106 2005 08 03.53186 22 45 46.64 -08 27 43.2 05PF23 568 Cq7106 2005 08 03.54753 22 45 46.59 -08 27 43.3 05PF23 568 Cq7106 2005 08 03.55276 22 45 46.55 -08 27 43.4 05PF23 568 Cq7106 2005 08 03.55799 22 45 46.53 -08 27 43.4 05PF23 568 Cq7106 2005 08 03.58940 22 45 46.41 -08 27 44.5 05PF23 568 Cq7106
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 0.03 0.00 -0.04
2 0.0000 -0.39 -0.03 -0.17 -0.20
3 0.0000 -0.55 0.14 0.22 0.19
4 0.0000 -0.76 0.26 0.09 0.06
5 0.0001 -1.85 -0.17 -0.22 -0.25
6 0.0003 -5.91 0.04 0.03 0.01
7 0.0003 -6.50 -0.22 0.16 0.14
8 0.0003 -6.68 -0.07 0.13 0.11
9 0.0027 -60.77 -0.16 -0.52 0.07
10 0.0027 -60.98 -0.04 -0.65 -0.06
11 0.0028 -62.97 -0.03 -0.81 -0.21
12 0.0028 -63.69 0.24 -0.63 -0.02
13 0.0028 -64.28 -0.01 -0.49 0.11
14 0.0028 -64.56 0.04 -0.38 0.22
15 0.0029 -66.62 -0.02 -0.73 -0.12
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.
05PF23 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