Orbit Fit and Astrometric record for 03OS33

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: 03OS33    
# Created Thu May 24 01:37:16 2012
# Orbit generated from Bernstein formalism
# Fitting   23 observations of   23
# Arc:  56.92d
# First observation: 2003/06/05
#  Last observation: 2003/08/01
Preliminary a, adot, b, bdot, g, gdot:
   0.000000   0.035943   0.000013  -0.012382   0.029519   0.000000
# Chi-squared of fit:     3.57 DOF:   40 RMS:  0.07
# Min/Max residuals:    -0.18    0.15
# Exact a, adot, b, bdot, g, gdot:
  1.949850E-05  3.413046E-02 -7.006325E-06 -1.222902E-02  2.869011E-02  8.594705E-03
# Covariance matrix:
  5.1264E-13 -2.0114E-11 -3.7336E-14 -1.6131E-12 -4.6267E-12 -1.3757E-10
 -2.0114E-11  4.1363E-09  2.3594E-11 -2.1291E-11  1.5042E-09  1.6354E-07
 -3.7336E-14  2.3594E-11  4.7183E-13 -3.2124E-12  9.5715E-12  1.2225E-09
 -1.6131E-12 -2.1291E-11 -3.2124E-12  4.3101E-11 -3.2611E-11 -8.3085E-09
 -4.6267E-12  1.5042E-09  9.5715E-12 -3.2611E-11  5.7751E-10  6.8111E-08
 -1.3757E-10  1.6354E-07  1.2225E-09 -8.3085E-09  6.8111E-08  9.0045E-06
#      lat0       lon0       xBary       yBary       zBary        JD0
   -6.293240  -30.090458    0.984319   -0.028446   -0.257900  2452796.099833
# Heliocentric elements and errors
Epoch:              2452790.5000  =  2003/05/31
Mean Anomaly:            9.58116 +/-     2.739
Argument of Peri:      163.17990 +/-    10.118
Long of Asc Node:      131.50375 +/-     0.062
Inclination:            20.74368 +/-     0.067
Eccentricity:         0.52539388 +/-    0.0731
Semi-Major Axis:     69.46871041 +/-    7.6587
Time of Perihelion: 2447161.9347 +/-    1312.5
Perihelion:          32.97027514 +/-    6.2462
Aphelion:           105.96714568 +/-   12.7391
Period (y)              579.0180 +/-     95.75
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           29.70515547 +/-    0.0251
Ecliptic Y          -18.34702769 +/-    0.0145
Ecliptic Z           -3.82093808 +/-    0.0032
Ecliptic XDOT         0.00222176 +/-    0.0002
Ecliptic YDOT         0.00246831 +/-    0.0001
Ecliptic ZDOT        -0.00124968 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   35.12277402 +/-    0.0226
Geocenter to KBO     34.85521552 +/-    0.0292
# Hcoef:  7.83

The following table shows the complete astrometric record for 03OS33. 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 (03OS33) followed by the observatory code and reference code for the source of the astrometry.

2003 06  05.59909  22 17 15.64   -17 23 08.4   22.7i 03OS33    568  Cs6950      
2003 06  06.59114  22 17 15.70   -17 23 27.0   22.7i 03OS33    568  Cs6950      
2003 06  07.59499  22 17 15.64   -17 23 45.9   22.8r 03OS33    568  Cs6950      
2003 06  24.54668  22 16 58.62   -17 30 29.7   23.0r 03OS33    568  Cs6950      
2003 06  24.55698  22 16 58.59   -17 30 30.0   23.0r 03OS33    568  Cs6950      
2003 06  24.56734  22 16 58.57   -17 30 30.3   23.1r 03OS33    568  Cs6950      
2003 07  04.53431  22 16 35.20   -17 35 29.5   22.8i 03OS33    568  Cs6950      
2003 07  04.55514  22 16 35.14   -17 35 30.1   22.7i 03OS33    568  Cs6950      
2003 07  04.56912  22 16 35.10   -17 35 30.5   22.6i 03OS33    568  Cs6950      
2003 07  22.54243  22 15 31.77   -17 45 51.6   22.9r 03OS33    568  Cs6950      
2003 07  22.55297  22 15 31.73   -17 45 52.0   22.8r 03OS33    568  Cs6950      
2003 07  22.56358  22 15 31.68   -17 45 52.3   22.8r 03OS33    568  Cs6950      
2003 07  31.46785  22 14 52.21   -17 51 23.8   22.7i 03OS33    568  Cs6950      
2003 07  31.51046  22 14 52.01   -17 51 25.4   22.6i 03OS33    568  Cs6950      
2003 07  31.52126  22 14 51.96   -17 51 25.8   23.3g 03OS33    568  Cs6950      
2003 07  31.52761  22 14 51.92   -17 51 26.2   23.5g 03OS33    568  Cs6950      
2003 07  31.53398  22 14 51.90   -17 51 26.4   23.4g 03OS33    568  Cs6950      
2003 07  31.53852  22 14 51.88   -17 51 26.5   22.8r 03OS33    568  Cs6950      
2003 07  31.55685  22 14 51.79   -17 51 27.1   22.7r 03OS33    568  Cs6950      
2003 07  31.56734  22 14 51.74   -17 51 27.5   22.9r 03OS33    568  Cs6950      
2003 08  01.49368  22 14 47.39   -17 52 02.5   22.8r 03OS33    568  Cs6950      
2003 08  01.50614  22 14 47.34   -17 52 03.0   22.8r 03OS33    568  Cs6950      
2003 08  01.51662  22 14 47.29   -17 52 03.3   22.9r 03OS33    568  Cs6950      

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     0.05
  2   0.0027     -5.91    -0.02     -17.66    -0.18
  3   0.0055    -13.52     0.13     -34.98     0.08
  4   0.0519   -386.26     0.15    -323.84     0.00
  5   0.0519   -386.77     0.01    -323.96     0.04
  6   0.0519   -387.14     0.01    -324.14     0.03
  7   0.0792   -806.69    -0.08    -482.93    -0.07
  8   0.0793   -807.71    -0.05    -483.18    -0.01
  9   0.0793   -808.39    -0.03    -483.35     0.03
 10   0.1285  -1876.22    -0.03    -737.94     0.05
 11   0.1286  -1876.90     0.03    -738.11     0.01
 12   0.1286  -1877.67     0.00    -738.13     0.12
 13   0.1530  -2522.76    -0.05    -845.81     0.04
 14   0.1531  -2525.99     0.00    -846.28     0.02
 15   0.1531  -2526.80     0.03    -846.40     0.02
 16   0.1531  -2527.48    -0.16    -846.57    -0.08
 17   0.1531  -2527.82    -0.01    -846.66    -0.10
 18   0.1532  -2528.12     0.04    -846.65    -0.04
 19   0.1532  -2529.54     0.04    -846.75     0.05
 20   0.1532  -2530.35     0.04    -846.87     0.05
 21   0.1558  -2600.87    -0.07    -857.34    -0.01
 22   0.1558  -2601.72     0.05    -857.55    -0.09
 23   0.1558  -2602.49     0.10    -857.58     0.00

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.

03OS33    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