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: 00GY146
# Created Sat May 4 01:10:15 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 17 observations of 17
# Arc: 14.97y
# First observation: 2000/04/03
# Last observation: 2015/03/23
# Chi-squared of fit: 53.11 DOF: 28 RMS: 0.31
# Min/Max residuals: -0.61 0.66
# Exact a, adot, b, bdot, g, gdot:
1.602876E-05 2.115647E-02 1.338289E-06 -9.955396E-04 2.279912E-02 6.555674E-05
# Covariance matrix:
1.5520E-13 -5.2016E-14 -1.1205E-15 1.9243E-15 -3.6289E-14 -1.2733E-13
-5.2016E-14 7.3707E-14 1.8877E-15 -3.2591E-15 1.1855E-14 2.1584E-13
-1.1205E-15 1.8877E-15 1.2989E-13 -1.0986E-14 6.3738E-16 5.8194E-15
1.9243E-15 -3.2591E-15 -1.0986E-14 3.7469E-15 -8.5769E-16 -1.0041E-14
-3.6289E-14 1.1855E-14 6.3738E-16 -8.5769E-16 6.9442E-13 5.4177E-14
-1.2733E-13 2.1584E-13 5.8194E-15 -1.0041E-14 5.4177E-14 6.6490E-13
# lat0 lon0 xBary yBary zBary JD0
0.189591 -170.548477 -0.080068 0.003112 -1.004109 2451637.870353
# Heliocentric elements and errors
Epoch: 2451638.5000 = 2000/04/04
Mean Anomaly: 164.47168 +/- 0.115
Argument of Peri: 10.82324 +/- 0.108
Long of Asc Node: 13.47810 +/- 0.000
Inclination: 2.70660 +/- 0.000
Eccentricity: 0.02610504 +/- 0.0001
Semi-Major Axis: 43.75583797 +/- 0.0061
Time of Perihelion: 2403339.1753 +/- 35.2
Perihelion: 42.61359015 +/- 0.0075
Aphelion: 44.89808579 +/- 0.0078
Period (y) 289.4424 +/- 0.06
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -44.23629957 +/- 0.0016
Ecliptic Y -7.44367812 +/- 0.0003
Ecliptic Z 0.14520938 +/- 0.0000
Ecliptic XDOT 0.00040287 +/- 0.0000
Ecliptic YDOT -0.00250076 +/- 0.0000
Ecliptic ZDOT -0.00011940 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 44.85843553 +/- 0.0016
Geocenter to KBO 43.86137524 +/- 0.0016
# Hcoef: 7.83
The following table shows the complete astrometric record for 00GY146. 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 (00GY146) followed by the observatory code and reference code for the source of the astrometry.
2000 04 03.36961 12 35 02.09 -03 34 15.3 24.2R 00GY146 568 Cb2885 2000 04 03.40451 12 35 01.96 -03 34 14.2 24.2R 00GY146 568 Cb2885 2000 04 03.44462 12 35 01.79 -03 34 13.1 24.2R 00GY146 568 Cb2885 2000 04 05.47872 12 34 53.15 -03 33 19.5 24.1R 00GY146 568 Cb2885 2000 04 05.52608 12 34 52.97 -03 33 17.6 24.1R 00GY146 568 Cb2885 2000 04 05.56623 12 34 52.79 -03 33 17.0 24.1R 00GY146 568 Cb2885 2000 05 07.36698 12 32 51.42 -03 20 42.4 24.5R 00GY146 568 Cb5789 2000 05 07.41047 12 32 51.30 -03 20 41.5 24.5R 00GY146 568 Cb5789 2001 02 17.54593 12 42 17.41 -04 23 50.0 23.4R 00GY146 568 Cc6646 2001 02 17.59356 12 42 17.26 -04 23 49.4 23.6R 00GY146 568 Cc6646 2001 02 18.54103 12 42 14.47 -04 23 31.7 00GY146 568 Cc6646 2001 03 24.37588 12 40 07.84 -04 10 23.3 23.3R 00GY146 695 Cc7846 2001 03 24.45951 12 40 07.49 -04 10 21.1 00GY146 695 Cc7846 2005 04 15.20682 12 56 10.57 -06 06 41.0 23.8R 00GY146 304 Cn3225 2005 04 15.24563 12 56 10.41 -06 06 39.8 00GY146 304 Cn3225 2015 03 23.36370 13 42 23.62 -11 18 48.8 23.8R 00GY146 695 C~1Q39 2015 03 23.42692 13 42 23.37 -11 18 47.3 00GY146 695 C~1Q3A
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 -0.42 0.00 -0.27
2 0.0001 0.00 -0.11 0.00 -0.10
3 0.0002 0.00 -0.06 0.00 -0.07
4 0.0058 0.00 -0.36 0.00 -0.34
5 0.0059 0.00 -0.01 0.00 0.31
6 0.0060 0.00 -0.13 0.00 -0.15
7 0.0931 0.00 -0.22 0.00 -0.61
8 0.0932 0.00 0.10 0.00 -0.56
9 0.8766 0.00 0.08 0.00 0.23
10 0.8767 0.00 -0.02 0.00 -0.04
11 0.8793 0.00 0.18 0.00 0.26
12 0.9720 0.00 0.54 0.00 0.66
13 0.9722 0.00 0.66 0.00 0.66
14 5.0317 0.00 -0.10 0.00 -0.04
15 5.0318 0.00 -0.02 0.00 0.16
16 14.9678 0.00 -0.02 0.00 -0.16
17 14.9680 0.00 -0.04 0.00 0.02
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.
00GY146 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 43.737 43.737 43.737 ecceobj 0.026 0.026 0.026 incobj 2.708 2.708 2.708 qmin 42.045 42.046 42.044 qmax 46.183 46.183 46.182 amean 44.025 44.025 44.025 amin 43.688 43.687 43.688 amax 44.378 44.377 44.378 emean 0.026 0.026 0.026 emin 0.010 0.010 0.010 emax 0.041 0.041 0.041 imean 2.840 2.840 2.840 imin 2.144 2.144 2.144 imax 3.393 3.393 3.393 excite_mean 0.056 0.056 0.056 fracstop 1.000 1.000 1.000 cjmean 3.098 3.098 3.098 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 178.7 178.8 178.7 kozaiamp 180.0 180.0 180.0