Orbit Fit and Astrometric record for 01OK108

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: 01OK108   
# Created Fri Apr 26 01:10:28 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     22 observations of     22
# Arc:  22.15y
# First observation: 1999/07/20
#  Last observation: 2021/09/12
# Chi-squared of fit:    44.78 DOF:     38 RMS:  0.25
# Min/Max residuals:    -0.42    0.77
# Exact a, adot, b, bdot, g, gdot:
  1.612944E-05  2.374961E-02  9.332826E-07 -8.216043E-04  2.432068E-02  7.568495E-04
# Covariance matrix:
  2.4937E-13 -8.0762E-14 -4.6443E-15  2.6330E-15 -1.3898E-14 -1.2990E-13
 -8.0762E-14  4.4561E-14  2.6682E-15 -1.5285E-15  2.7807E-14  7.5045E-14
 -4.6443E-15  2.6682E-15  1.2081E-13 -7.2685E-15  6.9329E-16  4.6941E-15
  2.6330E-15 -1.5285E-15 -7.2685E-15  1.1758E-15 -6.2192E-16 -2.6704E-15
 -1.3898E-14  2.7807E-14  6.9329E-16 -6.2192E-16  2.8909E-13  2.5414E-14
 -1.2990E-13  7.5045E-14  4.6941E-15 -2.6704E-15  2.5414E-14  1.3153E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.261656  -57.754879    0.096541   -0.004852   -1.009335  2451379.848853
# Heliocentric elements and errors
Epoch:              2451380.5000  =  1999/07/21
Mean Anomaly:           49.98854 +/-     0.080
Argument of Peri:      134.32528 +/-     0.086
Long of Asc Node:      114.78349 +/-     0.001
Inclination:             1.99703 +/-     0.000
Eccentricity:         0.03365409 +/-    0.0000
Semi-Major Axis:     43.03127844 +/-    0.0038
Time of Perihelion: 2437063.8068 +/-      22.8
Perihelion:          41.58309984 +/-    0.0041
Aphelion:            44.47945703 +/-    0.0043
Period (y)              282.2829 +/-      0.04
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           22.40290286 +/-    0.0005
Ecliptic Y          -35.67890027 +/-    0.0008
Ecliptic Z           -0.18770956 +/-    0.0000
Ecliptic XDOT         0.00230302 +/-    0.0000
Ecliptic YDOT         0.00136327 +/-    0.0000
Ecliptic ZDOT        -0.00009283 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   42.12965475 +/-    0.0007
Geocenter to KBO     41.11728509 +/-    0.0009
# Hcoef:  7.55

The following table shows the complete astrometric record for 01OK108. 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 (01OK108) followed by the observatory code and reference code for the source of the astrometry.

1999 07  20.34811  20 18 17.76   -19 54 51.8   23.3R 01OK108   568  Cf8906      
1999 07  20.37552  20 18 17.63   -19 54 52.2   23.2R 01OK108   568  Cf8906      
1999 07  20.40243  20 18 17.49   -19 54 52.7         01OK108   568  Cf8906      
2001 07  24.35455  20 29 14.23   -19 23 33.8   23.9R 01OK108   568  Cd3420      
2001 07  24.39547  20 29 14.02   -19 23 34.6   23.0R 01OK108   568  Cd3420      
2001 07  24.43635  20 29 13.81   -19 23 35.3   22.7R 01OK108   568  Cd3420      
2001 07  25.38578  20 29 09.18   -19 23 52.4   23.1R 01OK108   568  Cd3420      
2001 09  20.15725  20 25 15.55   -19 37 36.2   23.6R 01OK108   675  Ce0251      
2001 09  20.16155  20 25 15.53   -19 37 36.2   23.4R 01OK108   675  Ce0251      
2001 09  20.20371  20 25 15.43   -19 37 36.4   24.2R 01OK108   675  Ce0251      
2001 09  20.20785  20 25 15.42   -19 37 36.3   23.9R 01OK108   675  Ce0251      
2002 06  07.39777  20 38 01.59   -18 54 05.5   24. R 01OK108   675  Cf8906      
2002 06  07.42708  20 38 01.50   -18 54 06.0         01OK108   675  Cf8906      
2002 06  07.44869  20 38 01.40   -18 54 06.2         01OK108   675  Cf8906      
2002 06  08.42175  20 37 58.76   -18 54 16.8         01OK108   675  Cf8906      
2013 10  05.13939  21 29 46.54   -15 44 25.0   23.3R 01OK108   695  C~0zdD      
2013 10  06.11748  21 29 44.15   -15 44 36.3         01OK108   695  C~0zdD      
2013 10  07.14082  21 29 41.69   -15 44 46.7         01OK108   695  C~0zdD      
2013 10  07.22721  21 29 41.49   -15 44 48.1         01OK108   695  C~0zdD      
2021 09  12.147910 22 12 32.163  -12 22 45.26  23.5G 01OK108   G37  C~5535      
2021 09  12.205820 22 12 31.915  -12 22 46.67        01OK108   G37  C~5535      
2021 09  12.262550 22 12 31.672  -12 22 47.99        01OK108   G37  C~5535      

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    -0.07       0.00    -0.33
     2   0.0001      0.00     0.03       0.00    -0.27
     3   0.0001      0.00    -0.06       0.00    -0.32
     4   2.0123      0.00     0.04       0.00     0.04
     5   2.0124      0.00    -0.06       0.00    -0.03
     6   2.0126      0.00    -0.16       0.00    -0.00
     7   2.0152      0.00    -0.00       0.00    -0.32
     8   2.1706      0.00     0.12       0.00    -0.01
     9   2.1706      0.00    -0.02       0.00     0.02
    10   2.1707      0.00     0.12       0.00     0.19
    11   2.1707      0.00     0.13       0.00     0.32
    12   2.8831      0.00     0.39       0.00     0.09
    13   2.8832      0.00     0.26       0.00    -0.08
    14   2.8832      0.00    -0.34       0.00    -0.05
    15   2.8859      0.00    -0.04       0.00     0.13
    16  14.2116      0.00    -0.28       0.00     0.59
    17  14.2143      0.00    -0.01       0.00     0.17
    18  14.2171      0.00    -0.27       0.00     0.77
    19  14.2173      0.00    -0.14       0.00     0.27
    20  22.1487      0.00     0.13       0.00    -0.37
    21  22.1488      0.00     0.15       0.00    -0.42
    22  22.1490      0.00     0.17       0.00    -0.42

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.

01OK108    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        42.957    42.957    42.957
ecceobj         0.033     0.033     0.033
incobj          1.998     1.998     1.998
qmin           40.957    40.965    40.955
qmax           45.164    45.164    45.164
amean          42.989    42.989    42.989
amin           42.663    42.663    42.663
amax           43.322    43.322    43.322
emean           0.024     0.024     0.024
emin            0.004     0.004     0.005
emax            0.043     0.043     0.043
imean           1.409     1.409     1.409
imin            0.280     0.280     0.280
imax            2.109     2.109     2.109
excite_mean     0.037     0.037     0.037
fracstop        1.000     1.000     1.000
cjmean          3.088     3.088     3.088

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       179.5     179.4     179.4
kozaiamp        179.9     179.9     180.0