Orbit Fit and Astrometric record for 00QB226

The following information shows the result of the orbit fit based on Gary Bernstein's method. Most of the information should be self-explanatory.

# Object: 00QB226   
# Created Fri May  2 02:36:32 2008
# Orbit generated from Bernstein formalism
# Fitting    8 observations of    8
# Arc:   1.15d
# First observation: 2000/08/29
#  Last observation: 2000/08/30
# WARNING Fitting with energy constraint
# WARNING and with gdot fixed = 0
# Chi-squared of fit:     2.57 DOF:   12 RMS:  0.10
# Min/Max residuals:    -0.13    0.15
# Exact a, adot, b, bdot, g, gdot:
  1.456159E-05  2.140851E-02  1.332244E-06  1.134156E-03  2.250393E-02  0.000000E+00
# Covariance matrix:
  2.7630E-11  3.8389E-08 -5.5896E-14  1.1611E-11  6.2046E-09  0.0000E+00
  3.8389E-08  5.4161E-05 -7.8475E-11  1.6254E-08  8.7152E-06  0.0000E+00
 -5.5896E-14 -7.8475E-11  2.4068E-13 -8.3552E-11 -1.2659E-11  0.0000E+00
  1.1611E-11  1.6254E-08 -8.3552E-11  1.2255E-07  2.6259E-09  0.0000E+00
  6.2046E-09  8.7152E-06 -1.2659E-11  2.6259E-09  1.4056E-06  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  1.4997E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
   -1.711997  -22.175352    0.037531   -0.030220   -1.005438  2451785.587543
# Heliocentric elements and errors
Epoch:              2451780.5000  =  2000/08/24
Mean Anomaly:          355.30595 +/-   306.676
Argument of Peri:      336.17845 +/-    13.782
Long of Asc Node:        6.70506 +/-    11.153
Inclination:             3.45831 +/-     1.219
Eccentricity:         0.04666744 +/-    0.5535
Semi-Major Axis:     47.66179229 +/-   25.1959
Time of Perihelion: 2453347.6084 +/-  222566.5
Perihelion:          45.43753852 +/-   35.6767
Aphelion:            49.88604606 +/-   37.3005
Period (y)              329.0514 +/-    260.92
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           42.05463721 +/-    2.1668
Ecliptic Y          -17.17428768 +/-    0.8834
Ecliptic Z           -1.32751814 +/-    0.0699
Ecliptic XDOT         0.00097959 +/-    0.0014
Ecliptic YDOT         0.00241566 +/-    0.0009
Ecliptic ZDOT         0.00013807 +/-    0.0001
# Distances at JD0 (AU)
Heliocenter to KBO   45.44569257 +/-    2.0327
Geocenter to KBO     44.43668465 +/-    2.3410
# Hcoef:  6.65

The following table shows the complete astrometric record for 00QB226. 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 (00QB226) followed by the observatory code and reference code for the source of the astrometry.

2000 08  29.08680  22 40 34.66   -10 13 23.1         00QB226   809  Cb8401      
2000 08  29.17985  22 40 34.25   -10 13 25.2         00QB226   809  Cb8401      
2000 08  29.27935  22 40 33.83   -10 13 27.8         00QB226   809  Cb8401      
2000 08  29.33632  22 40 33.57   -10 13 29.1         00QB226   809  Cb8401      
2000 08  29.38881  22 40 33.35   -10 13 30.5         00QB226   809  Cb8401      
2000 08  30.06594  22 40 30.52   -10 13 47.1         00QB226   809  Cb8401      
2000 08  30.16189  22 40 30.11   -10 13 49.2   22.8R 00QB226   809  Cb8401      
2000 08  30.24026  22 40 29.76   -10 13 51.4         00QB226   809  Cb8401      

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     0.10       0.00    -0.11
  2   0.0003     -6.40     0.02       0.32     0.12
  3   0.0005    -13.12     0.06       0.23    -0.07
  4   0.0007    -17.17    -0.13       0.46     0.10
  5   0.0008    -20.70    -0.12       0.38    -0.03
  6   0.0027    -65.65     0.04       0.62    -0.10
  7   0.0029    -72.05     0.15       0.94     0.13
  8   0.0032    -77.67    -0.13       0.83    -0.05

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.

00QB226    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj       45.686    45.686    45.686
ecceobj        0.001     0.001     0.001
incobj         3.536     3.536     3.536
qmin          44.444    44.444    44.444
qmax          46.693    46.693    46.693
amean         45.508    45.508    45.508
amin          45.157    45.157    45.157
amax          45.860    45.860    45.860
emean          0.008     0.008     0.008
emin           0.000     0.000     0.000
emax           0.019     0.019     0.019
imean          3.883     3.883     3.883
imin           3.490     3.490     3.490
imax           4.267     4.267     4.267
fracstop       1.000     1.000     1.000
cjmean         3.114     3.114     3.114

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      176.5     176.6     176.6
kozaiamp       180.0     180.0     180.0