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: 06SE415 # Created Fri Apr 26 01:12:44 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 19 observations of 19 # Arc: 9.14y # First observation: 2006/09/18 # Last observation: 2015/11/08 # Chi-squared of fit: 37.11 DOF: 32 RMS: 0.25 # Min/Max residuals: -0.53 0.42 # Exact a, adot, b, bdot, g, gdot: 1.507327E-05 2.289584E-02 -4.654252E-06 -5.292431E-03 2.420992E-02 4.761837E-04 # Covariance matrix: 2.3863E-13 -1.9795E-13 -2.8194E-14 5.0461E-14 1.4498E-13 -9.5213E-13 -1.9795E-13 2.7043E-13 4.2340E-14 -7.1608E-14 -1.3686E-13 1.3582E-12 -2.8194E-14 4.2340E-14 1.1800E-13 -3.0532E-14 -1.1027E-14 2.1814E-13 5.0461E-14 -7.1608E-14 -3.0532E-14 3.1022E-14 5.0195E-14 -3.7875E-13 1.4498E-13 -1.3686E-13 -1.1027E-14 5.0195E-14 6.4727E-13 -8.9533E-13 -9.5213E-13 1.3582E-12 2.1814E-13 -3.7875E-13 -8.9533E-13 7.1663E-12 # lat0 lon0 xBary yBary zBary JD0 13.543023 -15.866490 -0.198209 0.231409 -0.960296 2453996.910694 # Heliocentric elements and errors Epoch: 2453996.5000 = 2006/09/18 Mean Anomaly: 74.29523 +/- 0.194 Argument of Peri: 56.46445 +/- 0.203 Long of Asc Node: 208.88634 +/- 0.001 Inclination: 18.54761 +/- 0.000 Eccentricity: 0.02900052 +/- 0.0001 Semi-Major Axis: 42.56561703 +/- 0.0067 Time of Perihelion: 2433062.8368 +/- 54.9 Perihelion: 41.33119209 +/- 0.0087 Aphelion: 43.80004198 +/- 0.0090 Period (y) 277.7133 +/- 0.07 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 39.62861553 +/- 0.0013 Ecliptic Y -11.06122420 +/- 0.0004 Ecliptic Z 9.67253509 +/- 0.0003 Ecliptic XDOT 0.00089779 +/- 0.0000 Ecliptic YDOT 0.00243324 +/- 0.0000 Ecliptic ZDOT -0.00056931 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 42.26504801 +/- 0.0012 Geocenter to KBO 41.30541862 +/- 0.0014 # Hcoef: 7.61
The following table shows the complete astrometric record for 06SE415. 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 (06SE415) followed by the observatory code and reference code for the source of the astrometry.
2006 09 18.40994 22 40 43.64 +06 15 53.5 23.8r 06SE415 568 C~1Q3U 2006 09 18.44287 22 40 43.49 +06 15 52.5 23.9r 06SE415 568 C~1Q3U 2006 09 18.47815 22 40 43.35 +06 15 51.1 23.5r 06SE415 568 C~1Q3U 2006 09 19.44822 22 40 39.30 +06 15 18.0 24.2r 06SE415 568 C~1Q3U 2006 09 20.25000 22 40 36.01 +06 14 51.1 23.7r 06SE415 568 C~1Q3U 2006 11 24.21024 22 38 10.45 +05 40 23.2 06SE415 695 C~1Q3U 2006 11 25.14804 22 38 10.83 +05 40 03.1 06SE415 695 C~1Q3U 2007 09 14.28157 22 46 22.70 +06 31 38.9 06SE415 568 C~1Q3U 2007 09 14.31239 22 46 22.61 +06 31 38.0 06SE415 568 C~1Q3U 2007 09 16.27938 22 46 14.15 +06 30 32.9 23.2R 06SE415 675 C~1Q3U 2007 09 16.32916 22 46 13.93 +06 30 31.4 23.1R 06SE415 675 C~1Q3U 2007 11 09.12887 22 43 32.07 +06 00 10.2 24.2r 06SE415 695 C~1Q3U 2007 11 09.19261 22 43 32.00 +06 00 08.4 23.8r 06SE415 695 C~1Q3U 2008 08 30.33054 22 52 45.81 +06 51 59.6 23.5r 06SE415 568 C~1Q3U 2008 08 30.36130 22 52 45.68 +06 51 58.8 23.4r 06SE415 568 C~1Q3U 2008 08 30.39232 22 52 45.53 +06 51 57.9 23.6r 06SE415 568 C~1Q3U 2008 08 31.31283 22 52 41.47 +06 51 31.6 06SE415 568 C~1Q3U 2015 11 08.09453 23 25 46.40 +07 39 43.5 24.7R 06SE415 G37 C~1dcV 2015 11 08.16155 23 25 46.29 +07 39 41.0 06SE415 G37 C~1dcV
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 0.22
2 0.0001 0.00 -0.26 0.00 0.33
3 0.0002 0.00 -0.10 0.00 0.13
4 0.0028 0.00 -0.10 0.00 -0.04
5 0.0050 0.00 0.26 0.00 0.42
6 0.1829 0.00 0.06 0.00 -0.35
7 0.1855 0.00 0.24 0.00 -0.24
8 0.9880 0.00 -0.53 0.00 -0.23
9 0.9881 0.00 0.15 0.00 -0.12
10 0.9935 0.00 0.10 0.00 -0.33
11 0.9936 0.00 0.05 0.00 -0.18
12 1.1409 0.00 0.16 0.00 -0.23
13 1.1411 0.00 0.28 0.00 -0.19
14 1.9491 0.00 0.04 0.00 0.31
15 1.9492 0.00 0.14 0.00 0.36
16 1.9493 0.00 -0.03 0.00 0.33
17 1.9518 0.00 -0.35 0.00 -0.14
18 9.1381 0.00 -0.28 0.00 0.21
19 9.1383 0.00 0.30 0.00 -0.23
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.
06SE415 quality flag:3 Type: SCATEXTD SCATEXTD SCATEXTD axisobj 42.797 42.797 42.797 ecceobj 0.027 0.027 0.027 incobj 18.479 18.479 18.479 qmin 40.933 40.932 40.933 qmax 44.510 44.510 44.509 amean 42.662 42.662 42.662 amin 42.334 42.334 42.334 amax 42.988 42.988 42.988 emean 0.025 0.025 0.025 emin 0.015 0.015 0.015 emax 0.036 0.036 0.036 imean 19.257 19.257 19.257 imin 18.831 18.831 18.831 imax 19.633 19.633 19.633 excite_mean 0.331 0.331 0.331 fracstop 1.000 1.000 1.000 cjmean 2.952 2.952 2.952 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 182.4 182.4 182.4 kozaiamp 179.9 179.9 179.9