Orbit Fit and Astrometric record for 00WT169

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: 00WT169   
# Created Fri May  2 02:36:32 2008
# Orbit generated from Bernstein formalism
# Fitting   22 observations of   22
# Arc:   4.29y
# First observation: 2000/11/23
#  Last observation: 2005/03/11
Preliminary a, adot, b, bdot, g, gdot:
   0.000224   0.020985   0.000005   0.000471   0.022710   0.000000
# Chi-squared of fit:   101.14 DOF:   38 RMS:  0.38
# Min/Max residuals:    -0.65    0.81
# Exact a, adot, b, bdot, g, gdot:
  1.617358E-05  2.137150E-02  3.067858E-06  4.830906E-04  2.277707E-02  3.368485E-04
# Covariance matrix:
  2.0746E-13 -1.3975E-13  6.6516E-16 -4.5753E-15  1.3189E-13 -1.7834E-12
 -1.3975E-13  4.9468E-13 -5.5361E-15  1.6092E-14  1.0437E-13  6.9746E-12
  6.6516E-16 -5.5361E-15  1.0311E-13 -4.0053E-14 -2.3509E-15 -8.4292E-14
 -4.5753E-15  1.6092E-14 -4.0053E-14  4.5759E-14  1.8506E-15  2.5252E-13
  1.3189E-13  1.0437E-13 -2.3509E-15  1.8506E-15  3.1673E-13  1.1787E-12
 -1.7834E-12  6.9746E-12 -8.4292E-14  2.5252E-13  1.1787E-12  1.0888E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
   -1.199993   68.368863    0.116004   -0.020552   -0.973776  2451871.955873
# Heliocentric elements and errors
Epoch:              2451870.5000  =  2000/11/22
Mean Anomaly:           56.36009 +/-     0.750
Argument of Peri:      259.80419 +/-     0.801
Long of Asc Node:      110.47974 +/-     0.012
Inclination:             1.74482 +/-     0.000
Eccentricity:         0.01612974 +/-    0.0004
Semi-Major Axis:     45.28025899 +/-    0.0050
Time of Perihelion: 2434447.1767 +/-     232.0
Perihelion:          44.54990020 +/-    0.0207
Aphelion:            46.01061777 +/-    0.0208
Period (y)              304.6994 +/-      0.05
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           16.65185986 +/-    0.0004
Ecliptic Y           41.67064547 +/-    0.0010
Ecliptic Z           -0.91931894 +/-    0.0000
Ecliptic XDOT        -0.00238050 +/-    0.0000
Ecliptic YDOT         0.00099017 +/-    0.0000
Ecliptic ZDOT         0.00005738 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   44.88398687 +/-    0.0009
Geocenter to KBO     43.90380088 +/-    0.0011
# Hcoef:  6.08

The following table shows the complete astrometric record for 00WT169. 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 (00WT169) followed by the observatory code and reference code for the source of the astrometry.

2000 11  23.45513  04 27 18.50   +20 30 57.6         00WT169   568  Cc3044      
2000 11  23.47774  04 27 18.42   +20 30 57.5         00WT169   568  Cc3044      
2000 11  23.50024  04 27 18.30   +20 30 57.2         00WT169   568  Cc3044      
2000 11  29.48449  04 26 48.99   +20 29 53.2   21.9R 00WT169   568  Cc3044      
2000 11  29.50227  04 26 48.88   +20 29 52.8   22.0R 00WT169   568  Cc3044      
2000 12  17.46296  04 25 22.31   +20 26 47.5   22.0R 00WT169   568  Cc4033      
2000 12  17.47846  04 25 22.24   +20 26 47.3   22.1R 00WT169   568  Cc4033      
2001 01  25.13017  04 23 02.56   +20 22 17.3   22.7R 00WT169   695  Cc6724      
2001 01  25.22623  04 23 02.33   +20 22 16.9         00WT169   695  Cc6724      
2001 02  16.89482  04 22 35.05   +20 21 54.9         00WT169   950  Cc6724      
2001 02  18.97751  04 22 34.96   +20 21 58.6         00WT169   950  Cc6724      
2001 02  20.26288  04 22 35.22   +20 22 00.5   22.6R 00WT169   568  Cc6724      
2001 02  21.23176  04 22 35.44   +20 22 02.9   22.7R 00WT169   568  Cc6724      
2002 01  09.35957  04 28 56.91   +20 36 52.5   22.3R 00WT169   568  Ce6590      
2002 01  09.39748  04 28 56.76   +20 36 51.8   22.2R 00WT169   568  Ce6590      
2002 01  14.20980  04 28 40.38   +20 36 22.6   22.5R 00WT169   568  Ce6590      
2002 01  14.22422  04 28 40.33   +20 36 22.5   22.4R 00WT169   568  Ce6590      
2002 01  14.23044  04 28 40.31   +20 36 22.5   22.3R 00WT169   568  Ce6590      
2002 11  06.52312  04 38 59.94   +20 58 51.4   22.0R 00WT169   568  Cl8320      
2002 11  06.56643  04 38 59.76   +20 58 51.1         00WT169   568  Cl8320      
2005 03  09.14215  04 43 01.31   +21 12 01.6         00WT169   G96  Cn1549      
2005 03  11.14357  04 43 04.33   +21 12 11.2         00WT169   G96  Cn1549      

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    -0.28       0.00    -0.56
  2   0.0001     -1.13     0.19       0.08    -0.49
  3   0.0001     -2.84     0.06       0.04    -0.53
  4   0.0165   -419.57     0.15       1.46    -0.15
  5   0.0166   -421.16    -0.18       1.31    -0.31
  6   0.0657  -1651.72     0.26      11.04    -0.16
  7   0.0658  -1652.72     0.29      11.00    -0.22
  8   0.1716  -3634.58    -0.31      61.15     0.67
  9   0.1719  -3637.84    -0.43      61.29     0.63
 10   0.2339  -4020.03    -0.24     102.24     0.81
 11   0.2396  -4020.67    -0.47     106.10     0.76
 12   0.2431  -4016.75     0.58     107.38    -0.43
 13   0.2458  -4013.31     0.37     109.24    -0.40
 14   1.1277   1420.45     0.24     135.93     0.53
 15   1.1278   1418.26     0.01     135.56     0.11
 16   1.1410   1186.53    -0.02     142.19     0.06
 17   1.1411   1185.82    -0.06     142.20     0.05
 18   1.1411   1185.54    -0.04     142.25     0.08
 19   1.9523   9986.14    -0.17     202.68    -0.14
 20   1.9524   9983.60    -0.03     202.74    -0.07
 21   4.2894  13451.33    -0.65     528.41    -0.37
 22   4.2948  13494.65     0.72     532.35     0.16

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.

00WT169    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj       45.240    45.240    45.240
ecceobj        0.017     0.017     0.017
incobj         1.745     1.745     1.745
qmin          43.484    43.489    43.485
qmax          46.588    46.573    46.597
amean         44.950    44.950    44.950
amin          44.604    44.604    44.606
amax          45.305    45.300    45.307
emean          0.016     0.016     0.016
emin           0.001     0.001     0.001
emax           0.028     0.028     0.028
imean          0.652     0.652     0.652
imin           0.091     0.091     0.091
imax           1.033     1.033     1.033
fracstop       1.000     1.000     1.000
cjmean         3.113     3.113     3.113

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      193.1     193.0     193.0
kozaiamp       179.9     179.9     180.0