Orbit Fit and Astrometric record for 00FH8

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: 00FH8     
# Created Sat May  4 01:10:12 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     21 observations of     21
# Arc:  18.13y
# First observation: 2000/03/29
#  Last observation: 2018/05/16
# Chi-squared of fit:    71.52 DOF:     36 RMS:  0.33
# Min/Max residuals:    -0.54    0.88
# Exact a, adot, b, bdot, g, gdot:
  1.436712E-05  2.111424E-02 -2.371956E-06 -7.639831E-04  2.283629E-02  2.744004E-04
# Covariance matrix:
  1.4677E-13 -9.5402E-14 -1.7493E-15  3.3440E-15  2.2861E-14 -2.5134E-13
 -9.5402E-14  1.7028E-13  3.3284E-15 -6.3510E-15 -3.1264E-14  4.7715E-13
 -1.7493E-15  3.3284E-15  1.0029E-13 -7.2079E-15 -6.4202E-16  9.4500E-15
  3.3440E-15 -6.3510E-15 -7.2079E-15  2.4176E-15  1.5061E-15 -1.8060E-14
  2.2861E-14 -3.1264E-14 -6.4202E-16  1.5061E-15  2.9394E-13 -1.1753E-13
 -2.5134E-13  4.7715E-13  9.4500E-15 -1.8060E-14 -1.1753E-13  1.3573E-12
#      lat0       lon0       xBary       yBary       zBary        JD0
    0.100574 -173.963785   -0.054452    0.001553   -1.004230  2451632.902433
# Heliocentric elements and errors
Epoch:              2451632.5000  =  2000/03/29
Mean Anomaly:          153.60656 +/-     0.119
Argument of Peri:       21.82862 +/-     0.113
Long of Asc Node:        8.81084 +/-     0.000
Inclination:             2.07827 +/-     0.000
Eccentricity:         0.03795445 +/-    0.0001
Semi-Major Axis:     43.30328465 +/-    0.0044
Time of Perihelion: 2407221.8694 +/-      35.0
Perihelion:          41.65973248 +/-    0.0051
Aphelion:            44.94683682 +/-    0.0053
Period (y)              284.9636 +/-      0.04
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -44.53333619 +/-    0.0010
Ecliptic Y           -4.76177483 +/-    0.0001
Ecliptic Z            0.07677598 +/-    0.0000
Ecliptic XDOT         0.00022720 +/-    0.0000
Ecliptic YDOT        -0.00251409 +/-    0.0000
Ecliptic ZDOT        -0.00009142 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   44.78724702 +/-    0.0010
Geocenter to KBO     43.78998186 +/-    0.0010
# Hcoef:  7.37

The following table shows the complete astrometric record for 00FH8. 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 (00FH8) followed by the observatory code and reference code for the source of the astrometry.

2000 03  29.40169  12 22 19.49   -02 18 17.9   22.7R 00FH8     568  Cb2555      
2000 03  29.44417  12 22 19.29   -02 18 16.8   22.9R 00FH8     568  Cb2555      
2000 03  29.48942  12 22 19.09   -02 18 15.6         00FH8     568  Cb2555      
2000 03  30.57157  12 22 14.47   -02 17 47.2         00FH8     568  Cb2555      
2000 03  30.58840  12 22 14.39   -02 17 46.3         00FH8     568  Cb2555      
2000 07  27.97379  12 19 49.79   -02 03 18.5   23.8R 00FH8     309  Cb7658      
2000 07  27.97934  12 19 49.80   -02 03 18.6   23.9R 00FH8     309  Cb7658      
2000 07  27.98518  12 19 49.82   -02 03 18.6   23.9R 00FH8     309  Cb7658      
2001 01  19.53225  12 30 20.64   -03 12 21.6   23.7R 00FH8     675  Cd0818      
2001 01  23.52126  12 30 15.68   -03 11 51.0   23.5R 00FH8     675  Cd0818      
2001 02  24.23987  12 28 55.59   -03 03 29.0         00FH8     309  Cd0818      
2001 02  24.29212  12 28 55.40   -03 03 27.8   23.5R 00FH8     309  Cd0818      
2001 02  24.33747  12 28 55.24   -03 03 26.8   23.7R 00FH8     309  Cd0818      
2001 04  27.31082  12 24 46.73   -02 37 14.0   23.2R 00FH8     568  Cd0818      
2001 04  27.39579  12 24 46.40   -02 37 12.0         00FH8     568  Cd0818      
2001 04  27.47426  12 24 46.10   -02 37 10.4         00FH8     568  Cd0818      
2002 02  11.23476  12 33 57.84   -03 38 32.5         00FH8     304  Ce8748      
2002 02  11.30224  12 33 57.64   -03 38 31.5   24.0R 00FH8     304  Ce8748      
2015 04  24.23586  13 26 42.78   -09 41 29.0   23.7R 00FH8     G37  C~1Re8      
2015 04  24.40514  13 26 42.05   -09 41 24.3         00FH8     G37  C~1Re8      
2018 05  16.413443 13 38 41.660  -10 59 04.39  24.2G 00FH8     T12  C~2end      

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     0.33
     2   0.0001      0.00    -0.04       0.00     0.28
     3   0.0002      0.00    -0.10       0.00     0.26
     4   0.0032      0.00    -0.35       0.00    -0.54
     5   0.0032      0.00    -0.46       0.00    -0.09
     6   0.3301      0.00    -0.01       0.00    -0.51
     7   0.3301      0.00    -0.11       0.00    -0.50
     8   0.3301      0.00    -0.08       0.00    -0.38
     9   0.8108      0.00     0.58       0.00    -0.21
    10   0.8217      0.00     0.16       0.00     0.20
    11   0.9085      0.00    -0.08       0.00    -0.37
    12   0.9087      0.00    -0.14       0.00    -0.32
    13   0.9088      0.00    -0.11       0.00    -0.31
    14   1.0785      0.00     0.44       0.00     0.17
    15   1.0787      0.00     0.13       0.00     0.26
    16   1.0789      0.00    -0.10       0.00     0.09
    17   1.8722      0.00     0.23       0.00     0.88
    18   1.8724      0.00    -0.00       0.00     0.76
    19  15.0687      0.00     0.01       0.00    -0.18
    20  15.0691      0.00     0.00       0.00     0.34
    21  18.1301      0.00    -0.08       0.00    -0.25

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.

00FH8    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        43.284    43.284    43.284
ecceobj         0.038     0.038     0.038
incobj          2.079     2.079     2.079
qmin           40.938    40.941    40.934
qmax           46.400    46.399    46.403
amean          43.555    43.555    43.556
amin           43.217    43.216    43.217
amax           43.906    43.909    43.906
emean           0.040     0.040     0.040
emin            0.022     0.022     0.022
emax            0.057     0.057     0.057
imean           2.350     2.350     2.350
imin            1.512     1.512     1.512
imax            3.103     3.103     3.103
excite_mean     0.058     0.058     0.058
fracstop        1.000     1.000     1.000
cjmean          3.092     3.092     3.092

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       186.0     186.0     186.0
kozaiamp        180.0     180.0     180.0