Orbit Fit and Astrometric record for 02FX6

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: 02FX6     
# Created Fri Apr 19 01:10:42 2024
# Orbit generated from Bernstein formalism
# Fitting      6 observations of      6
# Arc:  18.62d
# First observation: 2002/03/20
#  Last observation: 2002/04/08
# WARNING Fitting with energy constraint
# WARNING and with gdot fixed = 0
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# Chi-squared of fit:    21.94 DOF:      8 RMS:  0.34
# Min/Max residuals:    -0.78    0.76
# Exact a, adot, b, bdot, g, gdot:
  1.326321E-05  1.864402E-02 -4.387957E-06 -7.541921E-03  2.146820E-02  0.000000E+00
# Covariance matrix:
  3.0381E-11  4.0220E-08  5.1490E-14 -1.9024E-11  6.4370E-09  0.0000E+00
  4.0220E-08  5.3937E-05  6.9035E-11 -2.5507E-08  8.6305E-06  0.0000E+00
  5.1490E-14  6.9035E-11  3.7765E-13 -7.7465E-12  1.1047E-11  0.0000E+00
 -1.9024E-11 -2.5507E-08 -7.7465E-12  4.6059E-10 -4.0815E-09  0.0000E+00
  6.4370E-09  8.6305E-06  1.1047E-11 -4.0815E-09  1.3810E-06  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  1.3020E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.270758 -175.526835    0.078249   -0.004778   -0.993727  2452353.974243
# Heliocentric elements and errors
Epoch:              2452350.5000  =  2002/03/17
Mean Anomaly:            1.52485 +/-   167.446
Argument of Peri:      178.98180 +/-   233.344
Long of Asc Node:        3.71691 +/-     0.262
Inclination:            22.01680 +/-     7.833
Eccentricity:         0.05794166 +/-    0.5439
Semi-Major Axis:     50.49775336 +/-   26.4447
Time of Perihelion: 2451795.3241 +/-  192035.3
Perihelion:          47.57182959 +/-   37.0826
Aphelion:            53.42367714 +/-   39.2071
Period (y)              358.8528 +/-    281.89
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -47.43400180 +/-    2.5420
Ecliptic Y           -3.62744840 +/-    0.1986
Ecliptic Z           -0.22030853 +/-    0.0121
Ecliptic XDOT         0.00018156 +/-    0.0015
Ecliptic YDOT        -0.00237124 +/-    0.0008
Ecliptic ZDOT        -0.00096160 +/-    0.0001
# Distances at JD0 (AU)
Heliocenter to KBO   47.57301173 +/-    2.5346
Geocenter to KBO     46.58051303 +/-    2.5498
# Hcoef:  6.95

The following table shows the complete astrometric record for 02FX6. 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 (02FX6) followed by the observatory code and reference code for the source of the astrometry.

2002 03  20.47350  12 15 59.49   -02 01 34.8   23.5R 02FX6     568  Cf5861      
2002 03  20.52786  12 15 59.27   -02 01 33.4   23.8R 02FX6     568  Cf5861      
2002 03  20.56595  12 15 59.10   -02 01 32.4   23.7R 02FX6     568  Cf5861      
2002 03  22.47947  12 15 51.19   -02 00 49.9         02FX6     568  Cf5861      
2002 04  08.02916  12 14 43.27   -01 54 46.7   22.3R 02FX6     807  Ch1599      
2002 04  08.09013  12 14 43.05   -01 54 43.9         02FX6     807  Ch1599      

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     0.10       0.00    -0.24
     2   0.0001     -3.58     0.13      -0.02    -0.01
     3   0.0003     -6.32    -0.07      -0.12     0.07
     4   0.0055   -132.02    -0.18      -8.16     0.20
     5   0.0508  -1210.76     0.12     -78.93    -0.78
     6   0.0510  -1214.90    -0.10     -77.67     0.76

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.

02FX6    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