Orbit Fit and Astrometric record for 01XC255

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: 01XC255   
# Created Fri Apr 19 01:10:37 2024
# Orbit generated from Bernstein formalism
# Fitting      6 observations of      6
# Arc:  56.04d
# First observation: 2001/12/09
#  Last observation: 2002/02/03
Preliminary a, adot, b, bdot, g, gdot:
  -0.000000   0.068398   0.000001   0.000987   0.031698   0.000000
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# WARNING Fitting with energy constraint
# Chi-squared of fit:     2.45 DOF:      7 RMS:  0.11
# Min/Max residuals:    -0.23    0.15
# Exact a, adot, b, bdot, g, gdot:
  1.816053E-05  2.863026E-02  3.233969E-07  9.812185E-04  2.519253E-02 -5.053593E-03
# Covariance matrix:
  8.8185E-12  1.3016E-08  2.9407E-13 -9.2712E-13  2.0691E-09 -1.7462E-08
  1.3016E-08  2.0962E-05  4.7409E-10 -1.5820E-09  3.3290E-06 -2.8734E-05
  2.9407E-13  4.7409E-10  6.7749E-13 -5.1123E-12  7.5283E-11 -6.5248E-10
 -9.2712E-13 -1.5820E-09 -5.1123E-12  6.1140E-11 -2.5022E-10  2.5082E-09
  2.0691E-09  3.3290E-06  7.5283E-11 -2.5022E-10  5.2871E-07 -4.5563E-06
 -1.7462E-08 -2.8734E-05 -6.5248E-10  2.5082E-09 -4.5563E-06  4.1752E-05
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.287064  106.188118    0.470665   -0.004377   -0.858542  2452252.969033
# Heliocentric elements and errors
Epoch:              2452250.5000  =  2001/12/07
Mean Anomaly:          345.40784 +/-    14.031
Argument of Peri:       28.89502 +/-    11.223
Long of Asc Node:      113.65806 +/-     1.240
Inclination:             1.98370 +/-     0.306
Eccentricity:         0.41338589 +/-    0.4322
Semi-Major Axis:     65.06310274 +/-   41.0046
Time of Perihelion: 2460020.4394 +/-    1366.7
Perihelion:          38.16693413 +/-   37.0026
Aphelion:            91.95927135 +/-   64.4160
Period (y)              524.8200 +/-    496.13
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -10.85262968 +/-    0.3193
Ecliptic Y           39.08113739 +/-    1.1003
Ecliptic Z           -0.19887380 +/-    0.0057
Ecliptic XDOT        -0.00284372 +/-    0.0002
Ecliptic YDOT        -0.00139439 +/-    0.0008
Ecliptic ZDOT         0.00010960 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   40.56050322 +/-    1.0636
Geocenter to KBO     39.69431047 +/-    1.1457
# Hcoef:  7.53

The following table shows the complete astrometric record for 01XC255. 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 (01XC255) followed by the observatory code and reference code for the source of the astrometry.

2001 12  09.46829  07 10 04.987  +22 10 22.78        01XC255   568  Ce7056      
2001 12  09.55544  07 10 04.588  +22 10 23.48        01XC255   568  Ce7056      
2002 01  14.24544  07 07 01.094  +22 15 41.14  23.3R 01XC255   568  Ce7056      
2002 01  14.27270  07 07 00.939  +22 15 41.33  23.2R 01XC255   568  Ce7056      
2002 02  03.43082  07 05 20.61   +22 18 34.6   23.2R 01XC255   568  Cf2430      
2002 02  03.50406  07 05 20.27   +22 18 35.1         01XC255   568  Cf2430      

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    -0.04       0.00     0.06
     2   0.0002     -5.59     0.04       0.03     0.08
     3   0.0980  -2573.45     0.06      16.77    -0.15
     4   0.0980  -2575.61    -0.06      16.71    -0.23
     5   0.1532  -3979.16     0.02      31.02     0.15
     6   0.1534  -3983.90    -0.02      30.99     0.09

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.

01XC255    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