Orbit Fit and Astrometric record for 04UT10

The following information shows the result of the orbit fit based on Gary Bernstein's method. Most of the information should be self-explanatory.

# Object: 04UT10    
# Created Fri May  2 02:36:55 2008
# Orbit generated from Bernstein formalism
# Fitting    6 observations of    6
# Arc:  58.27d
# First observation: 2004/10/17
#  Last observation: 2004/12/14
Preliminary a, adot, b, bdot, g, gdot:
   0.000000   0.014613   0.000000  -0.003069   0.017287   0.000000
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# WARNING Fitting with energy constraint
# Chi-squared of fit:     3.14 DOF:    7 RMS:  0.13
# Min/Max residuals:    -0.23    0.26
# Exact a, adot, b, bdot, g, gdot:
  1.248280E-05  1.303115E-02 -2.739685E-06 -3.058847E-03  1.707635E-02 -4.128604E-03
# Covariance matrix:
  7.9490E-13  3.1344E-10 -6.5384E-15 -7.3915E-12  6.9759E-11 -1.1761E-09
  3.1344E-10  3.2315E-07 -6.6015E-12 -7.4551E-09  7.0744E-08 -1.4114E-06
 -6.5384E-15 -6.6015E-12  4.8463E-13 -2.9201E-12 -1.5421E-12 -1.5120E-11
 -7.3915E-12 -7.4551E-09 -2.9201E-12  2.3548E-10 -1.7517E-09 -2.1669E-08
  6.9759E-11  7.0744E-08 -1.5421E-12 -1.7517E-09  1.6105E-08 -2.9443E-08
 -1.1761E-09 -1.4114E-06 -1.5120E-11 -2.1669E-08 -2.9443E-08  1.3316E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
   -1.479888    9.881177   -0.240824   -0.024955   -0.970327  2453295.559443
# Heliocentric elements and errors
Epoch:              2453290.5000  =  2004/10/12
Mean Anomaly:          288.65451 +/-    99.710
Argument of Peri:      291.57490 +/-    46.377
Long of Asc Node:      183.94246 +/-     0.250
Inclination:            13.29970 +/-     0.522
Eccentricity:         0.29307151 +/-    0.7666
Semi-Major Axis:     60.10600261 +/-   31.1003
Time of Perihelion: 2487022.2761 +/-   39204.2
Perihelion:          42.49064551 +/-   51.0541
Aphelion:            77.72135971 +/-   61.1588
Period (y)              465.9990 +/-    361.68
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           58.58314853 +/-    0.4286
Ecliptic Y           10.45133870 +/-    0.0746
Ecliptic Z           -1.51256405 +/-    0.0112
Ecliptic XDOT        -0.00102431 +/-    0.0018
Ecliptic YDOT         0.00193543 +/-    0.0003
Ecliptic ZDOT        -0.00047307 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   59.52733509 +/-    0.4220
Geocenter to KBO     58.56052067 +/-    0.4352
# Hcoef:  7.16

The following table shows the complete astrometric record for 04UT10. 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 (04UT10) followed by the observatory code and reference code for the source of the astrometry.

2004 10  17.05870  00 38 38.83   +02 33 10.7         04UT10    304  Cn7976      
2004 10  17.09701  00 38 38.73   +02 33 10.0         04UT10    304  Cn7976      
2004 10  17.13526  00 38 38.58   +02 33 09.1         04UT10    304  Cn7976      
2004 12  12.31999  00 36 37.96   +02 19 36.1   24.7R 04UT10    568  Cn7976      
2004 12  13.33042  00 36 37.27   +02 19 31.1   24.8R 04UT10    568  Cn7976      
2004 12  14.32403  00 36 36.62   +02 19 27.1   24.4R 04UT10    568  Cn7976      

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    -0.09       0.00    -0.02
  2   0.0001     -1.65     0.26      -0.06    -0.04
  3   0.0002     -4.07    -0.17       0.00     0.06
  4   0.1540  -1985.83    -0.05     -38.38     0.11
  5   0.1568  -1997.31     0.09     -38.92    -0.23
  6   0.1595  -2007.84    -0.05     -38.78     0.12

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.

04UT10    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj       60.909    60.909    60.909
ecceobj        0.292     0.292     0.292
incobj        13.209    13.209    13.209
qmin          42.084    42.096    42.067
qmax          79.605    79.670    79.621
amean         60.422    60.421    60.421
amin          59.778    59.797    59.794
amax          61.182    61.198    61.188
emean          0.290     0.290     0.290
emin           0.280     0.279     0.279
emax           0.301     0.302     0.302
imean         13.157    13.157    13.157
imin          12.902    12.900    12.903
imax          13.488    13.486    13.490
fracstop       1.000     1.000     1.000
cjmean         3.138     3.138     3.138

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      170.9     170.9     170.9
kozaiamp       180.0     179.9     180.0