Orbit Fit and Astrometric record for 04FW164

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: 04FW164   
# Created Thu May 24 01:37:26 2012
# Orbit generated from Bernstein formalism
# Fitting   21 observations of   21
# Arc:   2.27y
# First observation: 2003/04/26
#  Last observation: 2005/08/02
Preliminary a, adot, b, bdot, g, gdot:
   0.000522   0.034807   0.000164   0.005468   0.031816   0.000000
# WARNING -- MRQMIN stopped after  17 iterations
# Chi-squared of fit:   179.54 DOF:   36 RMS:  0.52
# Min/Max residuals:    -1.17    1.13
# Exact a, adot, b, bdot, g, gdot:
  1.878175E-05  3.569791E-02 -2.529024E-06  5.724297E-03  3.088617E-02 -1.112925E-03
# Covariance matrix:
  4.7984E-13 -7.2035E-13  4.1493E-14 -1.0265E-13 -2.7130E-13 -7.0703E-12
 -7.2035E-13  1.9935E-12 -1.5574E-13  3.8791E-13  3.0179E-13  2.7005E-11
  4.1493E-14 -1.5574E-13  2.7186E-13 -1.8415E-13 -2.8950E-15 -2.3883E-12
 -1.0265E-13  3.8791E-13 -1.8415E-13  2.0585E-13  4.6098E-15  5.9654E-12
 -2.7130E-13  3.0179E-13 -2.8950E-15  4.6098E-15  7.1952E-13  3.7029E-14
 -7.0703E-12  2.7005E-11 -2.3883E-12  5.9654E-12  3.7029E-14  4.1712E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.266670 -164.236899   -0.346772   -0.004402   -0.945421  2452755.824823
# Heliocentric elements and errors
Epoch:              2452750.5000  =  2003/04/21
Mean Anomaly:          354.56411 +/-     0.167
Argument of Peri:        5.94600 +/-     0.234
Long of Asc Node:      197.96899 +/-     0.000
Inclination:             9.10963 +/-     0.001
Eccentricity:         0.16084274 +/-    0.0001
Semi-Major Axis:     39.66436032 +/-    0.0051
Time of Perihelion: 2454128.2390 +/-      42.3
Perihelion:          33.28463592 +/-    0.0053
Aphelion:            46.04408471 +/-    0.0067
Period (y)              249.8095 +/-      0.05
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -31.97664864 +/-    0.0009
Ecliptic Y           -9.38233200 +/-    0.0003
Ecliptic Z           -0.15075305 +/-    0.0000
Ecliptic XDOT         0.00094614 +/-    0.0000
Ecliptic YDOT        -0.00302414 +/-    0.0000
Ecliptic ZDOT         0.00050806 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   33.32501970 +/-    0.0008
Geocenter to KBO     32.37694786 +/-    0.0009
# Hcoef:  8.07

The following table shows the complete astrometric record for 04FW164. 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 (04FW164) followed by the observatory code and reference code for the source of the astrometry.

2003 04  26.32408  12 57 39.91   -06 26 58.6   22.7R 04FW164   568  Cq9909      
2003 04  26.36628  12 57 39.69   -06 26 57.1   22.6R 04FW164   568  Cq9909      
2003 04  26.40867  12 57 39.46   -06 26 55.6   22.5R 04FW164   568  Cq9909      
2004 03  20.57450  13 09 00.65   -07 17 45.3         04FW164   568  Cq9909      
2004 03  29.52259  13 08 13.60   -07 12 26.1   23.3R 04FW164   568  Cq9909      
2004 03  29.54560  13 08 13.43   -07 12 25.2   23.2R 04FW164   568  Cq9909      
2004 03  29.57409  13 08 13.29   -07 12 24.2   23.6R 04FW164   568  Cq9909      
2004 04  15.29003  13 06 42.28   -07 02 08.3         04FW164   675  Cq9909      
2004 04  15.33913  13 06 42.00   -07 02 06.2         04FW164   675  Cq9909      
2004 04  15.38135  13 06 41.76   -07 02 05.0         04FW164   675  Cq9909      
2004 04  16.24938  13 06 37.08   -07 01 32.4         04FW164   675  Cq9909      
2004 05  24.19250  13 03 43.16   -06 41 31.6         04FW164   695  Cq9909      
2004 05  24.24012  13 03 43.01   -06 41 30.8         04FW164   695  Cq9909      
2004 05  24.29308  13 03 42.83   -06 41 29.3         04FW164   695  Cq9909      
2005 07  08.28030  13 10 46.54   -07 01 35.5   22.9r 04FW164   568  Cq9909      
2005 08  01.97568  13 11 43.10   -07 06 17.5         04FW164   309  Cq9909      
2005 08  01.97898  13 11 43.12   -07 06 17.8         04FW164   309  Cq9909      
2005 08  01.98307  13 11 43.12   -07 06 17.8         04FW164   309  Cq9909      
2005 08  02.97488  13 11 46.72   -07 06 37.3         04FW164   309  Cq9909      
2005 08  02.97822  13 11 46.72   -07 06 37.8         04FW164   309  Cq9909      
2005 08  02.98225  13 11 46.73   -07 06 37.4         04FW164   309  Cq9909      

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     1.13
  2   0.0001     -3.60    -0.15       0.12     1.13
  3   0.0002     -7.35    -0.32       0.18     1.08
  4   0.9014  10541.23    -0.29    1064.44    -0.49
  5   0.9259   9770.48     0.52    1093.61    -0.52
  6   0.9260   9767.79    -0.11    1093.48    -0.71
  7   0.9261   9765.48     0.12    1093.61    -0.66
  8   0.9718   8275.53     0.25    1147.48    -1.03
  9   0.9720   8270.87     0.01    1147.84    -0.80
 10   0.9721   8267.10     0.03    1147.58    -1.17
 11   0.9745   8190.14    -0.27    1151.17    -0.46
 12   1.0784   5334.63     0.07    1272.05     0.12
 13   1.0785   5332.25     0.39    1271.93    -0.12
 14   1.0786   5329.20     0.33    1272.30     0.10
 15   2.2011  11634.95     0.57    2562.21     0.48
 16   2.2687  12524.12    -0.19    2620.60     0.62
 17   2.2687  12524.51     0.02    2620.44     0.45
 18   2.2687  12524.51    -0.21    2620.44     0.44
 19   2.2715  12581.70    -0.14    2622.70     0.35
 20   2.2715  12581.89    -0.14    2622.24    -0.12
 21   2.2715  12581.88    -0.39    2622.66     0.30

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.

04FW164    quality flag:3

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

axisobj        39.269    39.284    39.255
ecceobj         0.153     0.153     0.153
incobj          9.140     9.141     9.140
qmin           32.889    32.888    32.839
qmax           46.312    46.351    46.343
amean          39.456    39.456    39.456
amin           39.306    39.292    39.317
amax           39.614    39.627    39.602
emean           0.155     0.155     0.155
emin            0.139     0.139     0.138
emax            0.169     0.170     0.170
imean           9.917     9.900     9.940
imin            9.258     9.258     9.233
imax           10.637    10.583    10.662
excite_mean     0.232     0.232     0.232
fracstop        1.000     1.000     1.000
cjmean          2.991     2.991     2.991

libcent 0       180.6     180.3     180.2
libamp  0        79.3      84.8      73.6
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       179.9     183.3     181.8
kozaiamp        180.0     180.0     180.0