Orbit Fit and Astrometric record for 99CT153

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: 99CT153   
# Created Wed Nov 27 02:07:57 2024
# Orbit generated from Bernstein formalism
# Fitting      6 observations of      6
# Arc:   3.10y
# First observation: 1999/02/11
#  Last observation: 2002/03/20
Preliminary a, adot, b, bdot, g, gdot:
  -0.000001   0.024371   0.000003   0.001941   0.024810   0.000000
# Chi-squared of fit:     9.51 DOF:      6 RMS:  0.22
# Min/Max residuals:    -0.50    0.50
# Exact a, adot, b, bdot, g, gdot:
  1.521955E-05  2.508564E-02  1.451153E-06  2.011488E-03  2.492891E-02  1.220319E-02
# Covariance matrix:
  7.4530E-13  1.3628E-11 -5.4926E-14  1.3323E-12  3.9198E-12  2.1831E-10
  1.3628E-11  2.0778E-08 -8.4111E-11  2.0373E-09  3.9290E-09  3.3379E-07
 -5.4926E-14 -8.4111E-11  7.1837E-13 -8.3726E-12 -1.5902E-11 -1.3512E-09
  1.3323E-12  2.0373E-09 -8.3726E-12  1.9988E-10  3.8518E-10  3.2729E-08
  3.9198E-12  3.9290E-09 -1.5902E-11  3.8518E-10  7.4781E-10  6.3109E-08
  2.1831E-10  3.3379E-07 -1.3512E-09  3.2729E-08  6.3109E-08  5.3623E-06
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.188323  161.252115    0.317038   -0.003328   -0.941601  2451221.023253
# Heliocentric elements and errors
Epoch:              2451220.5000  =  1999/02/11
Mean Anomaly:           29.92023 +/-     6.948
Argument of Peri:      274.60487 +/-     0.196
Long of Asc Node:      163.10289 +/-     0.001
Inclination:             4.58096 +/-     0.002
Eccentricity:         0.51153507 +/-    0.0997
Semi-Major Axis:     59.01792089 +/-    8.6593
Time of Perihelion: 2437456.7519 +/-    1020.3
Perihelion:          28.82818458 +/-    7.2456
Aphelion:            89.20765721 +/-   14.3501
Period (y)              453.4027 +/-     99.79
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -38.76714449 +/-    0.0417
Ecliptic Y           13.49512582 +/-    0.0141
Ecliptic Z           -0.13177915 +/-    0.0001
Ecliptic XDOT        -0.00215699 +/-    0.0002
Ecliptic YDOT        -0.00216889 +/-    0.0001
Ecliptic ZDOT         0.00021651 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   41.04908377 +/-    0.0396
Geocenter to KBO     40.11406398 +/-    0.0440
# Hcoef:  7.80

The following table shows the complete astrometric record for 99CT153. 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 (99CT153) followed by the observatory code and reference code for the source of the astrometry.

1999 02  11.52251  10 50 31.45   +07 10 15.6   23.9R 99CT153   568  Ca4208      
1999 02  11.60642  10 50 31.06   +07 10 18.0   23.9R 99CT153   568  Ca4208      
1999 03  15.51731  10 48 05.41   +07 25 44.3   23.9R 99CT153   568  Ca4208      
1999 03  15.57045  10 48 05.15   +07 25 45.8   23.9R 99CT153   568  Ca4208      
2002 03  20.22230  11 03 48.298  +06 10 39.59  22.4R 99CT153   695              
2002 03  20.34667  11 03 47.694  +06 10 43.49        99CT153   695              

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     0.14       0.00    -0.04
     2   0.0002     -6.28    -0.15       0.02    -0.06
     3   0.0876  -2362.82     0.13      35.86     0.11
     4   0.0877  -2366.97    -0.13      35.78    -0.01
     5   3.1012  12351.03     0.50    1242.75    -0.03
     6   3.1015  12341.18    -0.50    1242.87     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.

99CT153    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