Orbit Fit and Astrometric record for 06UP321

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: 06UP321   
# Created Wed Nov 27 02:08:53 2024
# Orbit generated from Bernstein formalism
# Fitting      6 observations of      6
# Arc:  59.02d
# First observation: 2006/08/22
#  Last observation: 2006/10/20
Preliminary a, adot, b, bdot, g, gdot:
   0.000001   0.034657   0.000000  -0.003212   0.030244   0.000000
# WARNING Fitting with energy constraint
# Chi-squared of fit:     5.53 DOF:      7 RMS:  0.17
# Min/Max residuals:    -0.20    0.36
# Exact a, adot, b, bdot, g, gdot:
  1.770457E-05  3.219090E-02 -7.469820E-07 -3.104804E-03  2.963033E-02 -1.056293E-02
# Covariance matrix:
  1.1922E-12  1.9177E-09 -3.5966E-13 -7.6392E-11  3.6915E-10  1.1157E-08
  1.9177E-09  7.0991E-06 -1.2397E-09 -2.7666E-07  1.2842E-06  2.0630E-05
 -3.5966E-13 -1.2397E-09  7.1678E-13  4.5381E-11 -2.2725E-10 -4.3722E-09
 -7.6392E-11 -2.7666E-07  4.5381E-11  1.0834E-08 -5.0237E-08 -8.5269E-07
  3.6915E-10  1.2842E-06 -2.2725E-10 -5.0237E-08  2.3499E-07  4.4205E-06
  1.1157E-08  2.0630E-05 -4.3722E-09 -8.5269E-07  4.4205E-06  2.3709E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
    9.964305   11.097656    0.675673    0.130560   -0.742414  2453969.785404
# Heliocentric elements and errors
Epoch:              2453960.5000  =  2006/08/13
Mean Anomaly:          312.97286 +/-    28.459
Argument of Peri:      205.10283 +/-    25.774
Long of Asc Node:      250.57043 +/-     1.715
Inclination:            11.15195 +/-     0.189
Eccentricity:         0.35648356 +/-    0.4769
Semi-Major Axis:     40.45458190 +/-   13.8803
Time of Perihelion: 2466237.6079 +/-    3908.5
Perihelion:          26.03318852 +/-   21.2620
Aphelion:            54.87597529 +/-   26.9592
Period (y)              257.3118 +/-    132.43
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           33.48519578 +/-    0.5336
Ecliptic Y            5.87723622 +/-    0.1047
Ecliptic Z            5.83974023 +/-    0.0956
Ecliptic XDOT        -0.00146260 +/-    0.0014
Ecliptic YDOT         0.00273845 +/-    0.0004
Ecliptic ZDOT        -0.00045149 +/-    0.0002
# Distances at JD0 (AU)
Heliocenter to KBO   34.49496786 +/-    0.5186
Geocenter to KBO     33.74920407 +/-    0.5521
# Hcoef:  6.99

The following table shows the complete astrometric record for 06UP321. 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 (06UP321) followed by the observatory code and reference code for the source of the astrometry.

2006 08  22.28465  00 24 49.55   +13 32 32.9   21.9R 06UP321   807  C~00AI      
2006 08  23.20556  00 24 45.81   +13 32 19.4         06UP321   807  C~00AI      
2006 08  23.27405  00 24 45.53   +13 32 18.3         06UP321   807  C~00AI      
2006 10  19.25145  00 19 54.13   +13 03 06.6   22.2R 06UP321   695  Ct0648      
2006 10  19.35491  00 19 53.62   +13 03 02.6         06UP321   695  Ct0648      
2006 10  20.30911  00 19 48.80   +13 02 24.7         06UP321   695  Ct0648      

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    -0.11       0.00    -0.19
     2   0.0025    -55.37     0.02       9.54     0.14
     3   0.0027    -59.55     0.09      10.17     0.05
     4   0.1587  -4659.29    -0.18     125.40    -0.20
     5   0.1590  -4667.73     0.18     124.77    -0.18
     6   0.1616  -4747.52    -0.00     118.73     0.36

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.

06UP321    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