Orbit Fit and Astrometric record for 00CL104

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: 00CL104   
# Created Sun Dec 22 02:08:06 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     36 observations of     36
# Arc:  19.99y
# First observation: 2000/02/05
#  Last observation: 2020/02/01
# Chi-squared of fit:   103.43 DOF:     66 RMS:  0.30
# Min/Max residuals:    -0.49    0.71
# Exact a, adot, b, bdot, g, gdot:
  1.656988E-05  2.354295E-02  2.536682E-07  5.035267E-04  2.401849E-02  1.669470E-03
# Covariance matrix:
  1.3431E-13 -4.0111E-14  1.2556E-15 -7.9264E-16  1.4831E-14 -7.7925E-14
 -4.0111E-14  2.7942E-14 -9.1904E-16  5.9029E-16  2.7156E-14  5.7622E-14
  1.2556E-15 -9.1904E-16  7.2884E-14 -4.7846E-15 -7.1172E-16 -1.9561E-15
 -7.9264E-16  5.9029E-16 -4.7846E-15  7.0132E-16  5.0142E-16  1.2536E-15
  1.4831E-14  2.7156E-14 -7.1172E-16  5.0142E-16  1.8750E-13  4.7182E-14
 -7.7925E-14  5.7622E-14 -1.9561E-15  1.2536E-15  4.7182E-14  1.2248E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
    0.214017  150.916532    0.249716    0.003354   -0.956801  2451579.890013
# Heliocentric elements and errors
Epoch:              2451580.5000  =  2000/02/06
Mean Anomaly:           55.62620 +/-     0.028
Argument of Peri:      306.17178 +/-     0.033
Long of Asc Node:      140.91495 +/-     0.001
Inclination:             1.24711 +/-     0.000
Eccentricity:         0.07879142 +/-    0.0000
Semi-Major Axis:     44.36077788 +/-    0.0032
Time of Perihelion: 2434905.1852 +/-       8.5
Perihelion:          40.86552928 +/-    0.0032
Aphelion:            47.85602648 +/-    0.0036
Period (y)              295.4656 +/-      0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -37.09290835 +/-    0.0007
Ecliptic Y           20.92349946 +/-    0.0004
Ecliptic Z            0.15554468 +/-    0.0000
Ecliptic XDOT        -0.00147626 +/-    0.0000
Ecliptic YDOT        -0.00224573 +/-    0.0000
Ecliptic ZDOT         0.00005821 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   42.58752334 +/-    0.0006
Geocenter to KBO     41.63457708 +/-    0.0008
# Hcoef:  6.40

The following table shows the complete astrometric record for 00CL104. 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 (00CL104) followed by the observatory code and reference code for the source of the astrometry.

2000 02  05.38927  10 12 09.92   +11 20 55.1   22.0R 00CL104   695  Cb1114      
2000 02  05.49428  10 12 09.46   +11 20 57.9         00CL104   695  Cb1114      
2000 03  01.16806  10 10 16.35   +11 31 35.5   22.2R 00CL104   695  Cb1114      
2000 03  01.24778  10 10 16.01   +11 31 37.4         00CL104   695  Cb1114      
2000 12  21.64373  10 19 45.45   +10 39 34.1         00CL104   568  Cc3758      
2000 12  22.59385  10 19 43.86   +10 39 43.8   22.8R 00CL104   568  Cc3758      
2000 12  22.66463  10 19 43.72   +10 39 44.7         00CL104   568  Cc3758      
2001 02  21.18226  10 16 05.03   +11 00 54.4   22.0R 00CL104   688  Cc6636      
2001 02  21.22867  10 16 04.80   +11 00 55.5         00CL104   688  Cc6636      
2001 03  24.08038  10 13 51.31   +11 13 31.6   22.3  00CL104   304  Ce8743      
2001 03  24.09363  10 13 51.26   +11 13 32.0         00CL104   304  Ce8743      
2001 04  27.29029  10 12 19.69   +11 22 04.5   22.5R 00CL104   568  Cd0809      
2001 04  27.40763  10 12 19.52   +11 22 04.9         00CL104   568  Cd0809      
2002 02  04.55225  10 22 30.10   +10 26 07.5   22.0R 00CL104   568  Cf1711      
2002 02  04.60598  10 22 29.87   +10 26 08.9         00CL104   568  Cf1711      
2002 02  06.52553  10 22 21.55   +10 26 57.6         00CL104   568  Cf1711      
2002 02  06.57394  10 22 21.34   +10 26 58.7         00CL104   568  Cf1711      
2002 02  14.19816  10 21 47.33   +10 30 17.2   21.3R 00CL104   304   f1711      
2002 02  14.22052  10 21 47.22   +10 30 17.9         00CL104   304   f1711      
2003 03  31.151014 10 23 43.24   +10 21 10.0   22.1V 00CL104   645  C~2FZD      
2003 03  31.151843 10 23 43.25   +10 21 10.1   22.5V 00CL104   645  C~2FZD      
2003 03  31.154330 10 23 43.25   +10 21 10.1   24.9V 00CL104   645  C~2FZD      
2004 03  18.23124  10 29 36.06   +09 48 54.7   22.5R 00CL104   688  Ck2009      
2004 03  18.33010  10 29 35.62   +09 48 57.1         00CL104   688  Ck2009      
2007 02  15.37066  10 47 02.43   +08 10 20.4   22.2R 00CL104   688  Cu2276      
2007 02  15.44552  10 47 02.14   +08 10 22.7         00CL104   688  Cu2276      
2016 03  13.24257  11 28 54.42   +04 03 26.4   22.8R 00CL104   G37  C~1pPV      
2016 03  13.29163  11 28 54.20   +04 03 27.8         00CL104   G37  C~1pPV      
2018 04  24.35200  11 35 41.80   +03 22 45.8   22.5z 00CL104   T09  C~7b9t      
2018 04  24.39881  11 35 41.64   +03 22 46.5   22.7z 00CL104   T09  C~7b9t      
2018 04  24.44256  11 35 41.52   +03 22 47.5   22.3z 00CL104   T09  C~7b9t      
2018 04  24.48268  11 35 41.35   +03 22 48.7   23.2z 00CL104   T09  C~7b9t      
2019 03  08.38964  11 43 31.98   +02 33 38.7   23.1r 00CL104   T09  C~8CLS      
2019 03  08.40222  11 43 31.91   +02 33 39.1   23.1r 00CL104   T09  C~8CLS      
2019 03  08.43185  11 43 31.79   +02 33 39.7   23.1r 00CL104   T09  C~8CLS      
2020 02  01.590290 11 50 21.470  +01 50 23.71  22.9G 00CL104   T12  C~3q9S      

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    -0.20       0.00     0.09
     2   0.0003      0.00    -0.00       0.00     0.26
     3   0.0678      0.00     0.14       0.00     0.71
     4   0.0681      0.00     0.55       0.00     0.58
     5   0.8768      0.00     0.20       0.00    -0.44
     6   0.8794      0.00     0.31       0.00    -0.46
     7   0.8796      0.00     0.13       0.00    -0.30
     8   1.0453      0.00     0.25       0.00     0.62
     9   1.0454      0.00     0.05       0.00     0.49
    10   1.1299      0.00    -0.18       0.00     0.09
    11   1.1299      0.00    -0.17       0.00     0.21
    12   1.2235      0.00     0.27       0.00     0.23
    13   1.2239      0.00     0.28       0.00    -0.26
    14   1.9991      0.00    -0.47       0.00    -0.49
    15   1.9992      0.00    -0.39       0.00    -0.44
    16   2.0045      0.00    -0.26       0.00    -0.35
    17   2.0046      0.00    -0.18       0.00    -0.48
    18   2.0255      0.00    -0.34       0.00     0.02
    19   2.0255      0.00    -0.44       0.00     0.14
    20   3.1479      0.00    -0.24       0.00    -0.40
    21   3.1479      0.00    -0.04       0.00    -0.32
    22   3.1479      0.00     0.09       0.00    -0.37
    23   4.1146      0.00     0.44       0.00     0.23
    24   4.1148      0.00     0.10       0.00     0.23
    25   7.0280      0.00    -0.36       0.00    -0.06
    26   7.0282      0.00     0.23       0.00     0.24
    27  16.1009      0.00     0.29       0.00     0.20
    28  16.1010      0.00     0.24       0.00     0.22
    29  18.2148      0.00     0.10       0.00    -0.06
    30  18.2149      0.00    -0.07       0.00    -0.27
    31  18.2151      0.00     0.20       0.00    -0.12
    32  18.2152      0.00    -0.46       0.00     0.30
    33  19.0856      0.00     0.04       0.00     0.06
    34  19.0856      0.00    -0.19       0.00     0.11
    35  19.0857      0.00    -0.06       0.00    -0.13
    36  19.9896      0.00     0.07       0.00    -0.08

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.

00CL104    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        44.346    44.346    44.346
ecceobj         0.079     0.079     0.079
incobj          1.247     1.247     1.247
qmin           39.870    39.888    39.856
qmax           49.347    49.345    49.323
amean          44.475    44.475    44.475
amin           44.121    44.120    44.118
amax           44.856    44.861    44.858
emean           0.084     0.084     0.084
emin            0.068     0.068     0.068
emax            0.100     0.100     0.100
imean           1.356     1.356     1.356
imin            0.587     0.587     0.586
imax            2.028     2.027     2.027
excite_mean     0.088     0.088     0.088
fracstop        1.000     1.000     1.000
cjmean          3.098     3.098     3.098

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       207.4     207.5     207.4
kozaiamp        180.0     179.9     180.0