Orbit Fit and Astrometric record for 05EE296

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: 05EE296   
# Created Sun Dec 17 02:37:24 2017
# Orbit generated from Bernstein formalism
# Fitting   36 observations of   37
# Arc:   8.08y
# First observation: 2005/02/10
#  Last observation: 2013/03/13
Preliminary a, adot, b, bdot, g, gdot:
  -0.000322   0.020162   0.000010  -0.001059   0.021590   0.000000
# Chi-squared of fit:   158.17 DOF:   66 RMS:  0.37
# Min/Max residuals:    -1.42    0.94
# Exact a, adot, b, bdot, g, gdot:
  1.377397E-05  1.992800E-02 -1.342185E-06 -1.046316E-03  2.212005E-02 -1.053067E-03
# Covariance matrix:
  1.5876E-13 -1.3102E-13 -3.2154E-15  6.3430E-15  1.0365E-13 -7.7287E-13
 -1.3102E-13  1.6673E-13  4.7050E-15 -8.5918E-15 -8.1624E-14  1.0433E-12
 -3.2154E-15  4.7050E-15  6.0301E-14 -1.5391E-14 -1.3717E-15  3.1946E-14
  6.3430E-15 -8.5918E-15 -1.5391E-14  1.2467E-14  4.2017E-15 -5.7996E-14
  1.0365E-13 -8.1624E-14 -1.3717E-15  4.2017E-15  1.9608E-13 -5.1971E-13
 -7.7287E-13  1.0433E-12  3.1946E-14 -5.7996E-14 -5.1971E-13  7.0406E-12
#      lat0       lon0       xBary       yBary       zBary        JD0
    1.376277  137.830327   -0.061938    0.023690   -0.981304  2453411.813023
# Heliocentric elements and errors
Epoch:              2453410.5000  =  2005/02/09
Mean Anomaly:          235.53258 +/-     0.051
Argument of Peri:      286.27149 +/-     0.046
Long of Asc Node:      342.08155 +/-     0.002
Inclination:             3.28645 +/-     0.000
Eccentricity:         0.06678480 +/-    0.0001
Semi-Major Axis:     44.38782022 +/-    0.0039
Time of Perihelion: 2490756.7789 +/-      14.4
Perihelion:          41.42338856 +/-    0.0072
Aphelion:            47.35225188 +/-    0.0075
Period (y)              295.7358 +/-      0.04
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -34.27040954 +/-    0.0007
Ecliptic Y           30.95316493 +/-    0.0006
Ecliptic Z            1.08574534 +/-    0.0000
Ecliptic XDOT        -0.00156176 +/-    0.0000
Ecliptic YDOT        -0.00192067 +/-    0.0000
Ecliptic ZDOT        -0.00013253 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   46.19240449 +/-    0.0006
Geocenter to KBO     45.20784426 +/-    0.0009
# Hcoef:  6.79

The following table shows the complete astrometric record for 05EE296. 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 (05EE296) followed by the observatory code and reference code for the source of the astrometry.

2005 02  10.31228  09 22 50.86   +16 47 52.8   24.1g 05EE296   568  C~0VE0      
2005 02  10.39529  09 22 50.47   +16 47 54.6   23.8g 05EE296   568  C~0VE0      
2005 02  10.43481  09 22 50.29   +16 47 55.3   23.8g 05EE296   568  C~0VE0      
2005 03  09.24209  09 20 56.19   +16 56 11.2   22.8R 05EE296   695  Cn0309      
2005 03  09.33149  09 20 55.85   +16 56 12.6         05EE296   695  Cn0309      
2005 03  10.24246  09 20 52.42   +16 56 26.9         05EE296   695  Cn0309      
2005 03  12.195455 09 20 45.18   +16 56 56.8   22.7V 05EE296   645  C~2JxC      
2005 03  12.196285 09 20 45.18   +16 56 56.8   22.7V 05EE296   645  C~2JxC      
2005 03  12.198772 09 20 45.18   +16 56 56.8   23.7V 05EE296   645  C~2JxC      
2005 04  10.15339  09 19 25.92   +17 02 02.2   22.8R 05EE296   695  Cn3133      
2005 04  11.15418  09 19 24.26   +17 02 07.2         05EE296   695  Cn3133      
2005 04  12.15323  09 19 22.73   +17 02 12.1         05EE296   695  Cn3133      
2005 04  12.26136  09 19 22.54   +17 02 13.0   23.4i 05EE296   568  C~0VE0      
2005 04  12.34223  09 19 22.42   +17 02 13.5   23.7i 05EE296   568  C~0VE0      
2005 04  12.36980  09 19 22.38   +17 02 13.8   23.6i 05EE296   568  C~0VE0      
2005 04  13.16365  09 19 21.20   +17 02 16.9         05EE296   695  Cn3133      
2006 02  03.47735  09 27 50.77   +16 20 39.6         05EE296   568  C74769      
2006 02  06.32831  09 27 37.89   +16 21 39.0   22.9r 05EE296   568  C74769      
2006 02  06.36908  09 27 37.73   +16 21 39.9   22.5r 05EE296   568  C74769      
2006 02  06.40731  09 27 37.55   +16 21 40.7   23.0r 05EE296   568  C74769      
2006 03  02.22794  09 25 52.64   +16 29 34.0   22.8R 05EE296   695  Cr3594      
2006 03  02.28430  09 25 52.39   +16 29 34.9         05EE296   695  Cr3594      
2006 03  02.34040  09 25 52.16   +16 29 36.1         05EE296   695  Cr3594      
2006 04  26.01108  09 23 33.45   +16 38 38.5   21.7R 05EE296   807  Cr3594      
2006 04  28.01271  09 23 32.64   +16 38 37.1         05EE296   807  Cr3594      
2006 11  23.51542  09 35 40.62   +15 38 21.5         05EE296   695  C~0VE0      
2006 11  25.47075  09 35 40.11   +15 38 26.1         05EE296   695  C~0VE0      
2006 12  21.37965  09 35 02.50   +15 41 55.9   22.5R 05EE296   695  Ct5520      
2006 12  21.52007  09 35 02.13   +15 41 57.7         05EE296   695  Ct5520      
2007 02  18.30702  09 31 12.15   +16 00 34.9         05EE296   568  Cu1516      
2007 02  18.33757  09 31 12.00   +16 00 35.4         05EE296   568  Cu1516      
2007 02  18.34973  09 31 11.94   +16 00 35.7         05EE296   568  Cu1516      
2007 02  20.38766  09 31 02.78   +16 01 19.3   23.3R 05EE296   568  Cu1516      
2007 02  20.40850  09 31 02.69   +16 01 19.5   23.4R 05EE296   568  Cu1516      
2007 02  20.42607  09 31 02.62   +16 01 20.3   23.3R 05EE296   568  Cu1516      
2013 03  13.14623  09 56 01.77   +13 30 36.9   22.9R 05EE296   G37  C~0qSZ      
2013 03  13.19699  09 56 01.57   +13 30 37.9         05EE296   G37  C~0qSZ      

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     0.12
  2   0.0002     -5.88    -0.04      -0.01     0.18
  3   0.0003     -8.56     0.02      -0.14     0.09
  4   0.0737  -1719.62    -0.03     -30.66    -0.14
  5   0.0740  -1724.69     0.04     -30.82    -0.12
  6   0.0765  -1775.93     0.04     -32.24    -0.18
  7   0.0818  -1883.99    -0.18     -35.51    -0.36
  8   0.0818  -1883.99    -0.14     -35.51    -0.36
  9   0.0818  -1883.99     0.00     -35.51    -0.36
 10   0.1611  -3060.16    -0.18     -91.00     0.09
 11   0.1638  -3084.36    -0.19     -93.47    -0.18
 12   0.1666  -3106.76     0.35     -95.47     0.03
 13   0.1669  -3109.63    -0.11     -95.44     0.25
 14   0.1671  -3111.43    -0.02     -95.48     0.42
 15   0.1672  -3112.06    -0.03     -95.37     0.60
 16   0.1693  -3129.13    -0.05     -97.56     0.18
 17   0.9806   4606.64     0.21    -211.62     0.19
 18   0.9884   4411.88    -0.11    -213.38    -0.14
 19   0.9885   4409.41     0.25    -213.25     0.02
 20   0.9886   4406.70     0.19    -213.30    -0.01
 21   1.0538   2824.48     0.28    -235.53     0.06
 22   1.0540   2820.79     0.14    -235.80    -0.11
 23   1.0541   2817.27     0.16    -235.69     0.09
 24   1.2038    752.96    -0.12    -338.61     0.15
 25   1.2093    742.32     0.05    -343.53    -0.25
 26   1.7829  11849.36    -0.30    -461.15    -0.05
 27   1.7883  11840.88    -0.04    -459.17    -0.17
 28   1.8592  11257.23     0.05    -435.65    -0.33
 29   1.8596  11251.58    -0.08    -435.67    -0.40
 30   2.0205   7742.59     0.92    -438.65    -0.24
 31   2.0206   7740.38     0.80    -438.86    -0.42
 32   2.0206   7739.46     0.72    -438.85    -0.40
 33   2.0262   7600.19    -1.42    -439.46     0.94
 34   2.0263   7598.90    -1.30    -439.68     0.74
 35   2.0263   7597.68 (  -1.32)   -439.24 (   1.20)
 36   8.0844  31342.68    -0.00   -1786.86     0.01
 37   8.0846  31339.53     0.03   -1786.92     0.03

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.

05EE296    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        44.145    44.156    44.133
ecceobj         0.067     0.066     0.067
incobj          3.300     3.300     3.300
qmin           40.543    40.568    40.510
qmax           48.133    48.138    48.106
amean          44.205    44.217    44.194
amin           43.858    43.861    43.843
amax           44.579    44.590    44.557
emean           0.065     0.064     0.065
emin            0.049     0.048     0.049
emax            0.080     0.080     0.080
imean           4.262     4.263     4.261
imin            3.560     3.564     3.557
imax            4.817     4.818     4.826
excite_mean     0.099     0.098     0.099
fracstop        1.000     1.000     1.000
cjmean          3.092     3.092     3.092

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       182.8     182.6     183.2
kozaiamp        179.9     180.0     179.9