Orbit Fit and Astrometric record for 02GF32

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: 02GF32    
# Created Thu May 24 01:37:11 2012
# Orbit generated from Bernstein formalism
# Fitting   22 observations of   23
# Arc:   1.94y
# First observation: 2002/04/08
#  Last observation: 2004/03/16
Preliminary a, adot, b, bdot, g, gdot:
  -0.000085   0.022049  -0.000003  -0.001071   0.024018   0.000000
# Chi-squared of fit:    11.31 DOF:   38 RMS:  0.13
# Min/Max residuals:    -0.55    0.26
# Exact a, adot, b, bdot, g, gdot:
  1.460306E-05  2.222071E-02 -1.454537E-06 -1.081563E-03  2.423191E-02  3.820227E-03
# Covariance matrix:
  4.9610E-13 -3.9214E-15  2.0299E-15 -1.2403E-14  5.2732E-13  6.6620E-12
 -3.9214E-15  5.2278E-13  3.5431E-15 -2.2306E-14  2.7343E-13  1.2030E-11
  2.0299E-15  3.5431E-15  1.2378E-13 -9.9765E-14  4.1667E-15  1.3290E-13
 -1.2403E-14 -2.2306E-14 -9.9765E-14  1.7689E-13 -2.5741E-14 -8.3306E-13
  5.2732E-13  2.7343E-13  4.1667E-15 -2.5741E-14  8.0579E-13  1.3847E-11
  6.6620E-12  1.2030E-11  1.3290E-13 -8.3306E-13  1.3847E-11  4.4903E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
    0.144781 -138.051226    0.401334    0.002280   -0.919958  2452372.636773
# Heliocentric elements and errors
Epoch:              2452370.5000  =  2002/04/06
Mean Anomaly:          105.51246 +/-     0.176
Argument of Peri:       53.24323 +/-     0.151
Long of Asc Node:       44.31101 +/-     0.001
Inclination:             2.78421 +/-     0.001
Eccentricity:         0.17889792 +/-    0.0007
Semi-Major Axis:     39.23847712 +/-    0.0098
Time of Perihelion: 2426057.6494 +/-      42.8
Perihelion:          32.21879516 +/-    0.0291
Aphelion:            46.25815908 +/-    0.0303
Period (y)              245.7969 +/-      0.09
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -31.64397126 +/-    0.0012
Ecliptic Y          -27.89750050 +/-    0.0010
Ecliptic Z            0.10420330 +/-    0.0000
Ecliptic XDOT         0.00134865 +/-    0.0000
Ecliptic YDOT        -0.00215737 +/-    0.0000
Ecliptic ZDOT        -0.00012089 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   42.18556993 +/-    0.0011
Geocenter to KBO     41.26789020 +/-    0.0015
# Hcoef:  5.69

The following table shows the complete astrometric record for 02GF32. 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 (02GF32) followed by the observatory code and reference code for the source of the astrometry.

2002 04  08.13603  14 38 13.38   -15 16 57.6   21.1R 02GF32    807  Cf5154      
2002 04  08.22273  14 38 13.00   -15 16 55.9         02GF32    807  Cf5154      
2002 04  09.36795  14 38 08.02   -15 16 33.4         02GF32    807  Cf5154      
2002 06  07.30424  14 33 41.64   -14 56 18.3         02GF32    568  Cf8972      
2002 06  07.30783  14 33 41.63   -14 56 18.2         02GF32    568  Cf8972      
2002 06  07.31454  14 33 41.61   -14 56 18.1         02GF32    568  Cf8972      
2002 06  07.32242  14 33 41.57   -14 56 18.0         02GF32    568  Cf8972      
2002 06  07.32754  14 33 41.55   -14 56 17.9         02GF32    568  Cf8972      
2002 06  07.33125  14 33 41.54   -14 56 17.8         02GF32    568  Cf8972      
2002 06  07.33487  14 33 41.53   -14 56 17.7         02GF32    568  Cf8972      
2002 06  07.34156  14 33 41.50   -14 56 17.7         02GF32    568  Cf8972      
2002 06  07.34944  14 33 41.47   -14 56 17.5         02GF32    568  Cf8972      
2002 06  07.35457  14 33 41.45   -14 56 17.4         02GF32    568  Cf8972      
2002 06  12.20771  14 33 24.07   -14 54 59.1   21.7R 02GF32    688  Cf7381      
2002 06  12.30815  14 33 23.78   -14 54 56.3         02GF32    688  Cf7381      
2003 05  30.19331  14 39 10.40   -15 25 49.4   21.5R 02GF32    807  Ci2129      
2003 05  30.27877  14 39 10.02   -15 25 47.5         02GF32    807  Ci2129      
2003 05  31.11193  14 39 06.56   -15 25 32.1   21.4R 02GF32    807  Ci2129      
2003 05  31.14014  14 39 06.43   -15 25 31.4         02GF32    807  Ci2129      
2003 05  31.20217  14 39 06.17   -15 25 30.4         02GF32    807  Ci2129      
2003 06  01.03225  14 39 02.74   -15 25 15.1         02GF32    807  Ci2129      
2004 03  16.39418  14 49 24.84   -16 15 20.9   22.5R 02GF32    695  Ck4262      
2004 03  16.48630  14 49 24.56   -16 15 19.6         02GF32    695  Ck4262      

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    -0.02       0.00     0.15
  2   0.0002     -5.75    -0.02      -0.07     0.17
  3   0.0034    -81.24     0.04      -0.76     0.12
  4   0.1647  -4126.07    -0.04     -37.97     0.00
  5   0.1647  -4126.23     0.00     -37.92     0.05
  6   0.1648  -4126.54     0.08     -37.91     0.06
  7   0.1648  -4127.12    -0.05     -38.00    -0.01
  8   0.1648  -4127.43    -0.06     -37.99     0.00
  9   0.1648  -4127.60    -0.01     -37.94     0.05
 10   0.1648  -4127.77     0.03     -37.89     0.11
 11   0.1648  -4128.18     0.00     -38.03    -0.02
 12   0.1649  -4128.66    -0.02     -37.98     0.04
 13   0.1649  -4128.96    -0.03     -37.97     0.05
 14   0.1782  -4392.83     0.13     -42.10    -0.55
 15   0.1784  -4397.70 (   0.59)    -40.75 (   0.90)
 16   1.1418    947.98     0.10    -253.75    -0.18
 17   1.1421    942.17    -0.19    -253.62     0.02
 18   1.1444    889.83     0.11    -254.25    -0.10
 19   1.1444    887.82    -0.08    -254.16     0.02
 20   1.1446    883.94     0.01    -254.35    -0.12
 21   1.1469    832.04     0.03    -254.95    -0.24
 22   1.9391  10305.94     0.09    -429.79     0.12
 23   1.9394  10301.69    -0.09    -429.73     0.26

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.

02GF32    quality flag:3

Type:           3:2E      3:2E      3:2E

axisobj        39.079    39.108    39.051
ecceobj         0.178     0.180     0.177
incobj          2.792     2.792     2.792
qmin           32.216    32.163    32.274
qmax           47.124    47.123    47.096
amean          39.456    39.456    39.456
amin           39.258    39.277    39.237
amax           39.670    39.647    39.693
emean           0.175     0.176     0.173
emin            0.163     0.165     0.161
emax            0.188     0.189     0.187
imean           2.000     2.049     1.922
imin            1.457     1.532     1.285
imax            2.547     2.527     2.542
excite_mean     0.178     0.180     0.177
fracstop        1.000     1.000     1.000
cjmean          3.016     3.015     3.016

libcent 0       179.5     180.0     180.1
libamp  0        96.2      88.0     105.0
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       184.0     185.1     182.6
kozaiamp        180.0     180.0     180.0