Orbit Fit and Astrometric record for 06AA99

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: 06AA99    
# Created Wed Nov 27 02:08:48 2024
# Orbit generated from Bernstein formalism
# Fitting      5 observations of      5
# Arc:   1.06d
# First observation: 2006/01/05
#  Last observation: 2006/01/06
# WARNING Fitting with energy constraint
# WARNING and with gdot fixed = 0
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# Chi-squared of fit:    17.07 DOF:      6 RMS:  0.33
# Min/Max residuals:    -0.70    0.51
# Exact a, adot, b, bdot, g, gdot:
  1.797432E-05  4.124279E-02  1.039533E-05  2.882084E-02  4.015692E-02  0.000000E+00
# Covariance matrix:
  1.8071E-10  4.5681E-07 -1.5660E-12 -4.8621E-09  7.8361E-08  0.0000E+00
  4.5681E-07  1.1581E-03 -3.9683E-09 -1.2321E-05  1.9858E-04  0.0000E+00
 -1.5660E-12 -3.9683E-09  4.0836E-13 -8.4188E-11 -6.8054E-10  0.0000E+00
 -4.8621E-09 -1.2321E-05 -8.4188E-11  2.8929E-07 -2.1130E-06  0.0000E+00
  7.8361E-08  1.9858E-04 -6.8054E-10 -2.1130E-06  3.4054E-05  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  8.5213E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
    1.337134  129.677257    0.414356    0.020960   -0.892827  2453741.103774
# Heliocentric elements and errors
Epoch:              2453740.5000  =  2006/01/05
Mean Anomaly:          331.17973 +/-   355.616
Argument of Peri:       32.84373 +/-    63.456
Long of Asc Node:      126.92121 +/-     1.662
Inclination:            34.97591 +/-    22.504
Eccentricity:         0.03104889 +/-    0.6655
Semi-Major Axis:     26.51425481 +/-   15.0211
Time of Perihelion: 2457732.7082 +/-  148956.6
Perihelion:          25.69101676 +/-   22.8729
Aphelion:            27.33749286 +/-   23.4775
Period (y)              136.5298 +/-    116.02
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -16.15034592 +/-    2.3096
Ecliptic Y           20.11030125 +/-    2.7846
Ecliptic Z            0.58135835 +/-    0.0845
Ecliptic XDOT        -0.00213217 +/-    0.0019
Ecliptic YDOT        -0.00183686 +/-    0.0020
Ecliptic ZDOT         0.00196444 +/-    0.0003
# Distances at JD0 (AU)
Heliocenter to KBO   25.79914470 +/-    2.6081
Geocenter to KBO     24.90230662 +/-    3.6188
# Hcoef: 11.87

The following table shows the complete astrometric record for 06AA99. 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 (06AA99) followed by the observatory code and reference code for the source of the astrometry.

2006 01  05.60302  08 49 59.03   +19 06 56.5         06AA99    568  Cq7133      
2006 01  05.635206 08 49 58.81   +19 06 57.0         06AA99    T09  C~63RQ      
2006 01  05.65956  08 49 58.68   +19 06 59.2         06AA99    568  Cq7133      
2006 01  06.63678  08 49 51.73   +19 07 44.1   25.5R 06AA99    568  Cq7133      
2006 01  06.65830  08 49 51.59   +19 07 45.0   25.8R 06AA99    568  Cq7133      

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    -0.36       0.00     0.20
     2   0.0001     -3.14     0.04      -0.36    -0.70
     3   0.0002     -5.50     0.34       1.27     0.51
     4   0.0028   -112.44    -0.12      18.05     0.01
     5   0.0029   -114.60     0.10      18.38    -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.

06AA99    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