Orbit Fit and Astrometric record for 04MS8

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: 04MS8     
# Created Sun Dec 22 02:08:40 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     21 observations of     21
# Arc:  20.27y
# First observation: 2004/06/24
#  Last observation: 2024/10/01
# Chi-squared of fit:    28.91 DOF:     36 RMS:  0.21
# Min/Max residuals:    -0.34    0.78
# Exact a, adot, b, bdot, g, gdot:
  2.162073E-05  4.940718E-02  4.363160E-06  1.071519E-02  3.732226E-02  2.605441E-03
# Covariance matrix:
  1.1752E-13 -6.7186E-15  6.2407E-15 -7.7473E-16  6.1291E-14 -1.2167E-14
 -6.7186E-15  1.1895E-14 -1.5604E-14  1.3505E-15  2.6577E-14  2.0049E-14
  6.2407E-15 -1.5604E-14  1.1197E-13 -1.0429E-14 -2.1996E-14 -3.2915E-14
 -7.7473E-16  1.3505E-15 -1.0429E-14  1.2080E-15  1.4539E-15  2.9654E-15
  6.1291E-14  2.6577E-14 -2.1996E-14  1.4539E-15  1.7533E-13  2.0308E-14
 -1.2167E-14  2.0049E-14 -3.2915E-14  2.9654E-15  2.0308E-14  4.4355E-14
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.812176  -74.852159    0.207239   -0.014087   -0.996984  2453180.936473
# Heliocentric elements and errors
Epoch:              2453180.5000  =  2004/06/24
Mean Anomaly:            6.01727 +/-     0.001
Argument of Peri:      344.75517 +/-     0.000
Long of Asc Node:      288.31770 +/-     0.000
Inclination:            12.26567 +/-     0.000
Eccentricity:         0.29577337 +/-    0.0000
Semi-Major Axis:     39.27738829 +/-    0.0000
Time of Perihelion: 2451677.6727 +/-       0.3
Perihelion:          27.66018270 +/-    0.0001
Aphelion:            50.89459387 +/-    0.0001
Period (y)              246.1626 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X            7.05782922 +/-    0.0000
Ecliptic Y          -26.87490255 +/-    0.0000
Ecliptic Z           -0.37963695 +/-    0.0000
Ecliptic XDOT         0.00354892 +/-    0.0000
Ecliptic YDOT         0.00074488 +/-    0.0000
Ecliptic ZDOT         0.00078336 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   27.78877484 +/-    0.0000
Geocenter to KBO     26.79365839 +/-    0.0000
# Hcoef:  8.26

The following table shows the complete astrometric record for 04MS8. 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 (04MS8) followed by the observatory code and reference code for the source of the astrometry.

2004 06  24.43573  19 06 09.38   -23 23 09.4         04MS8     568  C~0Uqy      
2004 06  24.46335  19 06 09.18   -23 23 09.5         04MS8     568  C~0Uqy      
2004 06  25.45812  19 06 01.98   -23 23 15.1   23.4g 04MS8     568  C~0Uqy      
2004 06  25.45953  19 06 01.95   -23 23 15.1   23.1g 04MS8     568  C~0Uqy      
2004 06  25.48101  19 06 01.81   -23 23 15.4   22.7g 04MS8     568  C~0Uqy      
2004 06  25.48243  19 06 01.80   -23 23 15.3   22.9g 04MS8     568  C~0Uqy      
2004 06  25.49954  19 06 01.66   -23 23 15.4   22.9g 04MS8     568  C~0Uqy      
2004 06  25.50096  19 06 01.65   -23 23 15.2   22.8g 04MS8     568  C~0Uqy      
2005 06  11.46244  19 19 27.69   -22 24 22.2         04MS8     568  C~0Uqy      
2005 06  12.51301  19 19 21.02   -22 24 28.4         04MS8     568  C~0Uqy      
2005 06  12.55269  19 19 20.77   -22 24 28.7         04MS8     568  C~0Uqy      
2006 07  03.43985  19 28 35.70   -21 26 55.5   22.6r 04MS8     568  C~0Uqy      
2006 07  04.43937  19 28 28.52   -21 27 04.6   23.0r 04MS8     568  C~0Uqy      
2006 10  22.10888  19 21 59.64   -21 30 45.0         04MS8     675  C~0Uqy      
2006 10  23.11314  19 22 03.22   -21 30 34.0         04MS8     675  C~0Uqy      
2006 10  24.10993  19 22 06.87   -21 30 21.9         04MS8     675  C~0Uqy      
2013 10  05.10812  20 34 45.07   -14 02 50.8   22.4R 04MS8     695  C~0zdZ      
2013 10  06.09907  20 34 43.47   -14 03 00.9         04MS8     695  C~0zdZ      
2024 10  01.101420 22 10 44.043  -01 22 12.75  23.4G 04MS8     G37  C~8Gif      
2024 10  01.144690 22 10 43.843  -01 22 13.90        04MS8     G37  C~8Gif      
2024 10  01.186980 22 10 43.665  -01 22 15.46        04MS8     G37  C~8Gif      

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    -0.16       0.00     0.02
     2   0.0001      0.00    -0.11       0.00     0.08
     3   0.0028      0.00    -0.00       0.00     0.09
     4   0.0028      0.00    -0.29       0.00     0.10
     5   0.0029      0.00    -0.01       0.00    -0.08
     6   0.0029      0.00    -0.00       0.00     0.03
     7   0.0029      0.00    -0.20       0.00     0.02
     8   0.0029      0.00    -0.19       0.00     0.23
     9   0.9638      0.00     0.78       0.00    -0.25
    10   0.9667      0.00     0.00       0.00    -0.08
    11   0.9668      0.00     0.10       0.00    -0.14
    12   2.0233      0.00    -0.15       0.00     0.04
    13   2.0260      0.00    -0.27       0.00    -0.08
    14   2.3263      0.00    -0.01       0.00     0.21
    15   2.3290      0.00     0.52       0.00    -0.29
    16   2.3318      0.00     0.25       0.00     0.11
    17   9.2804      0.00    -0.34       0.00     0.04
    18   9.2831      0.00     0.12       0.00    -0.11
    19  20.2701      0.00     0.03       0.00    -0.11
    20  20.2703      0.00    -0.08       0.00     0.17
    21  20.2704      0.00     0.07       0.00     0.00

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.

04MS8    quality flag:3

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

axisobj        39.222    39.222    39.222
ecceobj         0.295     0.295     0.295
incobj         12.261    12.261    12.261
qmin           27.038    27.039    27.036
qmax           52.791    52.796    52.786
amean          39.455    39.455    39.455
amin           38.881    38.881    38.873
amax           40.121    40.137    40.144
emean           0.297     0.298     0.294
emin            0.282     0.283     0.280
emax            0.316     0.316     0.316
imean          13.945    13.953    14.090
imin           13.341    13.486    13.634
imax           14.550    14.448    14.689
excite_mean     0.383     0.383     0.382
fracstop        1.000     1.000     1.000
cjmean          2.884     2.884     2.884

libcent 0       179.6     179.4     180.6
libamp  0       125.6     127.6     127.3
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       179.3     177.5     175.4
kozaiamp        180.0     180.0     180.0