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: 00FY53
# Created Wed Nov 27 02:08:03 2024
# Orbit generated from Bernstein formalism
# Fitting 10 observations of 10
# Arc: 34.99d
# First observation: 2000/03/31
# Last observation: 2000/05/05
Preliminary a, adot, b, bdot, g, gdot:
0.000001 0.018209 -0.000000 -0.009103 0.026326 0.000000
# WARNING MRQMIN stopped after 13 iterations -- oscilliatory solution
# WARNING Fitting with energy constraint
# WARNING MRQMIN stopped after 15 iterations -- oscilliatory solution
# WARNING MRQMIN stopped after 13 iterations -- oscilliatory solution
# Chi-squared of fit: 13.14 DOF: 15 RMS: 0.20
# Min/Max residuals: -0.32 0.47
# Exact a, adot, b, bdot, g, gdot:
1.668443E-05 2.763790E-02 -5.407994E-06 -9.102630E-03 2.785937E-02 1.409926E-03
# Covariance matrix:
3.4911E-11 6.0235E-08 -1.3603E-12 -3.6205E-11 9.8989E-09 5.9242E-08
6.0235E-08 1.0617E-04 -2.4342E-09 -5.8435E-08 1.7432E-05 9.8646E-05
-1.3603E-12 -2.4342E-09 4.1780E-13 -2.9278E-12 -3.9925E-10 -2.0782E-09
-3.6205E-11 -5.8435E-08 -2.9278E-12 1.3564E-10 -9.6593E-09 -8.1156E-08
9.8989E-09 1.7432E-05 -3.9925E-10 -9.6593E-09 2.8625E-06 1.6267E-05
5.9242E-08 9.8646E-05 -2.0782E-09 -8.1156E-08 1.6267E-05 1.2047E-04
# lat0 lon0 xBary yBary zBary JD0
0.680246 -152.854417 0.275603 0.011266 -0.967858 2451635.052973
# Heliocentric elements and errors
Epoch: 2451630.5000 = 2000/03/27
Mean Anomaly: 68.05196 +/- 120.713
Argument of Peri: 104.93993 +/- 132.410
Long of Asc Node: 28.72295 +/- 0.725
Inclination: 18.28262 +/- 6.411
Eccentricity: 0.04497164 +/- 0.5041
Semi-Major Axis: 37.41768986 +/- 18.0222
Time of Perihelion: 2435827.0461 +/- 111048.7
Perihelion: 35.73495502 +/- 25.5361
Aphelion: 39.10042470 +/- 26.6556
Period (y) 228.8883 +/- 165.37
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -32.91869345 +/- 1.9397
Ecliptic Y -16.56932312 +/- 0.9944
Ecliptic Z 0.42598349 +/- 0.0259
Ecliptic XDOT 0.00110034 +/- 0.0006
Ecliptic YDOT -0.00247824 +/- 0.0012
Ecliptic ZDOT -0.00089273 +/- 0.0001
# Distances at JD0 (AU)
Heliocenter to KBO 36.85599421 +/- 1.7892
Geocenter to KBO 35.89456557 +/- 2.1799
# Hcoef: 8.92
The following table shows the complete astrometric record for 00FY53. 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 (00FY53) followed by the observatory code and reference code for the source of the astrometry.
2000 03 31.55223 13 41 46.02 -09 49 17.9 24.2R 00FY53 568 Cb4248 2000 03 31.57664 13 41 45.91 -09 49 17.8 24.2R 00FY53 568 Cb4248 2000 04 06.54861 13 41 14.89 -09 46 52.1 24.1R 00FY53 568 Cb4248 2000 04 06.59084 13 41 14.66 -09 46 50.4 24.2R 00FY53 568 Cb4248 2000 04 06.61263 13 41 14.55 -09 46 50.4 24.3R 00FY53 568 Cb4248 2000 05 05.493892 13 38 42.18 -09 35 00.7 00FY53 568 C~5V7b 2000 05 05.499141 13 38 42.16 -09 35 00.6 00FY53 568 C~5V7b 2000 05 05.515383 13 38 42.05 -09 35 00.5 00FY53 568 C~5V7b 2000 05 05.520191 13 38 42.03 -09 34 59.8 00FY53 568 C~5V7b 2000 05 05.538121 13 38 41.93 -09 34 59.8 00FY53 568 C~5V7b
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 -0.21 0.00 0.05
2 0.0001 -1.55 0.20 -0.49 -0.32
3 0.0164 -481.79 0.08 -29.32 -0.12
4 0.0165 -485.57 -0.21 -28.95 0.47
5 0.0166 -487.09 0.07 -29.54 -0.01
6 0.0957 -2844.63 0.13 -179.68 0.08
7 0.0957 -2844.94 0.23 -179.70 0.10
8 0.0957 -2846.49 -0.05 -180.19 -0.31
9 0.0957 -2847.02 -0.20 -179.64 0.27
10 0.0958 -2848.40 -0.17 -180.18 -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.
00FY53 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