Orbit Fit and Astrometric record for 00SU331

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: 00SU331   
# Created Wed Nov 27 02:08:07 2024
# Orbit generated from Bernstein formalism
# Fitting      6 observations of      6
# Arc:   1.14d
# First observation: 2000/09/23
#  Last observation: 2000/09/24
# WARNING Fitting with energy constraint
# WARNING and with gdot fixed = 0
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# Chi-squared of fit:     2.79 DOF:      8 RMS:  0.12
# Min/Max residuals:    -0.13    0.23
# Exact a, adot, b, bdot, g, gdot:
  1.544975E-05  2.941266E-02  9.458601E-07  1.199252E-03  2.806690E-02  0.000000E+00
# Covariance matrix:
  1.3918E-10  2.4518E-07  8.3033E-12  1.5269E-08  7.2452E-08  0.0000E+00
  2.4518E-07  4.3362E-04  1.4673E-08  2.6983E-05  1.2803E-04  0.0000E+00
  8.3033E-12  1.4673E-08  8.6626E-13  7.8761E-10  4.3338E-09  0.0000E+00
  1.5269E-08  2.6983E-05  7.8761E-10  1.8062E-06  7.9695E-06  0.0000E+00
  7.2452E-08  1.2803E-04  4.3338E-09  7.9695E-06  3.7816E-05  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  2.9094E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
   -2.303600   59.438727    0.855139   -0.020852   -0.513864  2451810.957343
# Heliocentric elements and errors
Epoch:              2451810.5000  =  2000/09/23
Mean Anomaly:          302.00894 +/-    22.067
Argument of Peri:       15.76794 +/-    83.008
Long of Asc Node:      102.95366 +/-    14.181
Inclination:             3.21524 +/-     0.776
Eccentricity:         0.02727585 +/-    0.6360
Semi-Major Axis:     36.66993821 +/-   20.7577
Time of Perihelion: 2464875.8850 +/-  329216.8
Perihelion:          35.66973460 +/-   30.8481
Aphelion:            37.67014181 +/-   31.6009
Period (y)              222.0616 +/-    188.55
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           19.10412638 +/-    3.9662
Ecliptic Y           30.66776857 +/-    6.7163
Ecliptic Z           -1.43205648 +/-    0.3138
Ecliptic XDOT        -0.00247563 +/-    0.0015
Ecliptic YDOT         0.00146794 +/-    0.0016
Ecliptic ZDOT         0.00011705 +/-    0.0001
# Distances at JD0 (AU)
Heliocenter to KBO   36.15979064 +/-    6.0695
Geocenter to KBO     35.62916056 +/-    7.8063
# Hcoef:  8.94

The following table shows the complete astrometric record for 00SU331. 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 (00SU331) followed by the observatory code and reference code for the source of the astrometry.

2000 09  23.45660  03 51 01.33   +17 46 48.6         00SU331   568  Cc1431      
2000 09  23.51348  03 51 01.16   +17 46 48.1   24.3R 00SU331   568  Cc1431      
2000 09  23.58921  03 51 00.97   +17 46 47.2   24.4R 00SU331   568  Cc1431      
2000 09  24.47004  03 50 58.78   +17 46 37.9   24.2R 00SU331   568  Cc1431      
2000 09  24.52751  03 50 58.63   +17 46 37.4   24.2R 00SU331   568  Cc1431      
2000 09  24.59204  03 50 58.48   +17 46 36.8   24.3R 00SU331   568  Cc1431      

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     0.23       0.00    -0.06
     2   0.0002     -2.48    -0.12       0.03     0.10
     3   0.0004     -5.32    -0.11      -0.28    -0.03
     4   0.0028    -37.86    -0.13      -2.72    -0.07
     5   0.0029    -40.06    -0.09      -2.75     0.02
     6   0.0031    -42.29     0.22      -2.88     0.04

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.

00SU331    quality flag:0

Type:      ERR2LARGE ERR2LARGE ERR2LARGE

axisobj         0.000     0.000     0.000
ecceobj        -1.000    -1.000    -1.000
incobj         -1.000    -1.000    -1.000
qmin            0.000     0.000     0.000
qmax            0.000     0.000     0.000
amean           0.000     0.000     0.000
amin            0.000     0.000     0.000
amax            0.000     0.000     0.000
emean           0.000     0.000     0.000
emin            0.000     0.000     0.000
emax            0.000     0.000     0.000
imean           0.000     0.000     0.000
imin            0.000     0.000     0.000
imax            0.000     0.000     0.000
excite_mean     0.000     0.000     0.000
fracstop        0.000     0.000     0.000
cjmean          0.000     0.000     0.000

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         0.0       0.0       0.0
kozaiamp          0.0       0.0       0.0