Orbit Fit and Astrometric record for 02AO217

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: 02AO217   
# Created Tue Sep  2 01:08:17 2025
# Orbit generated from Bernstein formalism
# Fitting      6 observations of      6
# Arc:   1.05d
# First observation: 2002/01/10
#  Last observation: 2002/01/11
# WARNING Fitting with energy constraint
# WARNING and with gdot fixed = 0
# Chi-squared of fit:     2.23 DOF:      8 RMS:  0.11
# Min/Max residuals:    -0.16    0.21
# Exact a, adot, b, bdot, g, gdot:
  1.681070E-05  2.734401E-02  5.796844E-07  7.469817E-04  2.667590E-02  0.000000E+00
# Covariance matrix:
  3.6268E-11  6.0155E-08 -7.4190E-14 -1.0502E-10  9.6706E-09  0.0000E+00
  6.0155E-08  1.0121E-04 -1.2441E-10 -1.7617E-07  1.6220E-05  0.0000E+00
 -7.4190E-14 -1.2441E-10  3.3797E-13 -1.0993E-10 -1.9966E-11  0.0000E+00
 -1.0502E-10 -1.7617E-07 -1.0993E-10  1.3082E-07 -2.8269E-08  0.0000E+00
  9.6706E-09  1.6220E-05 -1.9966E-11 -2.8269E-08  2.6028E-06  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  2.4979E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.451514   98.025115   -0.202355   -0.007624   -0.957526  2452284.727217
# Heliocentric elements and errors
Epoch:              2452280.5000  =  2002/01/06
Mean Anomaly:            9.95259 +/-   314.012
Argument of Peri:      333.70042 +/-    19.884
Long of Asc Node:      114.01183 +/-     9.235
Inclination:             1.62750 +/-     0.934
Eccentricity:         0.03087937 +/-    0.5707
Semi-Major Axis:     39.65525451 +/-   20.9946
Time of Perihelion: 2449758.8603 +/-  261975.0
Perihelion:          38.43072511 +/-   30.4325
Aphelion:            40.87978391 +/-   31.3142
Period (y)              249.7234 +/-    198.32
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           -5.56651249 +/-    0.3163
Ecliptic Y           38.04418583 +/-    2.2449
Ecliptic Z           -0.29539045 +/-    0.0179
Ecliptic XDOT        -0.00278757 +/-    0.0009
Ecliptic YDOT        -0.00039157 +/-    0.0016
Ecliptic ZDOT         0.00007688 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   38.45040172 +/-    2.2217
Geocenter to KBO     37.48702101 +/-    2.2672
# Hcoef:  8.23

The following table shows the complete astrometric record for 02AO217. 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 (02AO217) followed by the observatory code and reference code for the source of the astrometry.

2002 01  10.226474 06 34 49.59   +22 44 44.0   23.7R 02AO217   T09  C~90G3      
2002 01  10.252909 06 34 49.45   +22 44 44.2         02AO217   T09  C~90G3      
2002 01  10.274636 06 34 49.33   +22 44 44.3         02AO217   T09  C~90G3      
2002 01  11.229347 06 34 43.90   +22 44 49.2         02AO217   T09  C~90G3      
2002 01  11.251160 06 34 43.79   +22 44 49.4         02AO217   T09  C~90G3      
2002 01  11.273172 06 34 43.67   +22 44 49.8         02AO217   T09  C~90G3      

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    -0.12       0.00    -0.03
     2   0.0001     -1.95     0.03       0.08     0.03
     3   0.0001     -3.61     0.10       0.08     0.01
     4   0.0027    -78.88    -0.16       0.46    -0.15
     5   0.0028    -80.41     0.04       0.57    -0.07
     6   0.0029    -82.09     0.11       0.87     0.21

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.

02AO217    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