Orbit Fit and Astrometric record for 04DG64

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: 04DG64    
# Created Wed Dec 25 02:08:30 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     51 observations of     51
# Arc:  14.38y
# First observation: 2003/12/24
#  Last observation: 2018/05/12
# Chi-squared of fit:    16.92 DOF:     96 RMS:  0.10
# Min/Max residuals:    -0.32    0.24
# Exact a, adot, b, bdot, g, gdot:
  1.515505E-05  2.352953E-02 -4.493804E-07 -8.990026E-04  2.394598E-02  6.952403E-04
# Covariance matrix:
  2.5766E-13  2.0719E-14 -2.9651E-15 -1.0402E-15  1.6141E-13  9.8866E-14
  2.0719E-14  4.5191E-14 -8.8032E-16 -1.6115E-15  8.2104E-14  1.4575E-13
 -2.9651E-15 -8.8032E-16  1.5667E-13 -1.2901E-14 -4.6428E-15 -2.5321E-15
 -1.0402E-15 -1.6115E-15 -1.2901E-14  1.3450E-15 -2.7587E-15 -5.3830E-15
  1.6141E-13  8.2104E-14 -4.6428E-15 -2.7587E-15  2.8239E-13  2.5578E-13
  9.8866E-14  1.4575E-13 -2.5321E-15 -5.3830E-15  2.5578E-13  4.8605E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
    2.191734  168.702948    0.954111    0.008727   -0.226318  2452998.045148
# Heliocentric elements and errors
Epoch:              2452998.5000  =  2003/12/25
Mean Anomaly:           12.06341 +/-     0.054
Argument of Peri:      121.37130 +/-     0.059
Long of Asc Node:       33.02388 +/-     0.001
Inclination:             3.04722 +/-     0.000
Eccentricity:         0.03596556 +/-    0.0001
Semi-Major Axis:     43.53018351 +/-    0.0034
Time of Perihelion: 2449483.2865 +/-      15.8
Perihelion:          41.96459615 +/-    0.0040
Aphelion:            45.09577087 +/-    0.0042
Period (y)              287.2063 +/-      0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -40.96029758 +/-    0.0009
Ecliptic Y            9.15701137 +/-    0.0002
Ecliptic Z            1.59705627 +/-    0.0000
Ecliptic XDOT        -0.00061300 +/-    0.0000
Ecliptic YDOT        -0.00262810 +/-    0.0000
Ecliptic ZDOT        -0.00009952 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   42.00174995 +/-    0.0009
Geocenter to KBO     41.76067167 +/-    0.0009
# Hcoef:  7.36

The following table shows the complete astrometric record for 04DG64. 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 (04DG64) followed by the observatory code and reference code for the source of the astrometry.

2003 12  24.544405 11 21 54.45   +06 29 08.2         04DG64    T14  C~89L7      
2003 12  24.611265 11 21 54.41   +06 29 08.7         04DG64    T14  C~89L7      
2004 02  22.38330  11 19 13.54   +06 48 06.7   23.3R 04DG64    695  Ck0899      
2004 02  22.42483  11 19 13.36   +06 48 08.1         04DG64    695  Ck0899      
2004 02  26.35815  11 18 56.05   +06 49 59.0   23.3R 04DG64    695  Ck0899      
2004 02  26.43653  11 18 55.71   +06 50 01.3         04DG64    695  Ck0899      
2004 02  27.31905  11 18 51.77   +06 50 26.1         04DG64    695  Ck0899      
2004 03  15.21148  11 17 35.19   +06 58 24.1   24.0R 04DG64    695  Ck4349      
2004 03  15.29066  11 17 34.83   +06 58 26.7         04DG64    695  Ck4349      
2013 05  12.116886 11 58 31.793  +01 59 54.20  23.8r 04DG64    W84  C~8Gic      
2014 04  21.984629 12 04 29.842  +01 17 57.19  22.6z 04DG64    W84  C~8Gic      
2014 04  21.987519 12 04 29.832  +01 17 57.26  22.5z 04DG64    W84  C~8Gic      
2014 04  21.993267 12 04 29.810  +01 17 57.41  22.4z 04DG64    W84  C~8Gic      
2014 04  22.009290 12 04 29.748  +01 17 57.73  22.5z 04DG64    W84  C~8Gic      
2014 04  22.012158 12 04 29.743  +01 17 57.98  23.0z 04DG64    W84  C~8Gic      
2014 04  22.015021 12 04 29.726  +01 17 57.88  23.5z 04DG64    W84  C~8Gic      
2014 04  22.017898 12 04 29.717  +01 17 57.95  23.7z 04DG64    W84  C~8Gic      
2015 03  20.457985 12 11 44.87   +00 27 26.9         04DG64    T09  C~89L7      
2015 03  20.496906 12 11 44.69   +00 27 28.0         04DG64    T09  C~89L7      
2016 04  02.38656  12 15 39.10   -00 02 11.7   23.2i 04DG64    T09  C~89TZ      
2016 04  02.41462  12 15 38.99   -00 02 10.9   23.3i 04DG64    T09  C~89TZ      
2016 04  02.43920  12 15 38.87   -00 02 10.4   23.2i 04DG64    T09  C~89TZ      
2016 04  02.46363  12 15 38.76   -00 02 09.7   23.3i 04DG64    T09  C~89TZ      
2016 04  02.46633  12 15 38.75   -00 02 09.7   23.3i 04DG64    T09  C~89TZ      
2016 04  02.48823  12 15 38.65   -00 02 09.0   23.1i 04DG64    T09  C~89TZ      
2016 04  02.49902  12 15 38.61   -00 02 08.7   23.3i 04DG64    T09  C~89TZ      
2016 04  02.52059  12 15 38.51   -00 02 08.2   23.2i 04DG64    T09  C~89TZ      
2016 04  04.34312  12 15 30.49   -00 01 18.0   24.6g 04DG64    T09  C~89TZ      
2016 04  04.38515  12 15 30.30   -00 01 17.0   24.5g 04DG64    T09  C~89TZ      
2016 04  04.38727  12 15 30.29   -00 01 16.8   24.7g 04DG64    T09  C~89TZ      
2016 04  04.40435  12 15 30.20   -00 01 16.3   24.7g 04DG64    T09  C~89TZ      
2016 04  04.41084  12 15 30.19   -00 01 16.1   24.3g 04DG64    T09  C~89TZ      
2016 04  05.428310 12 15 25.73   -00 00 48.5         04DG64    T09  C~89L7      
2016 04  05.546249 12 15 25.20   -00 00 45.3         04DG64    T09  C~89L7      
2016 04  08.50449  12 15 12.35   +00 00 34.5   23.9r 04DG64    T09  C~89TZ      
2016 04  08.51156  12 15 12.32   +00 00 34.6   24.0r 04DG64    T09  C~89TZ      
2016 04  08.51792  12 15 12.28   +00 00 34.8   23.8r 04DG64    T09  C~89TZ      
2016 04  08.52425  12 15 12.26   +00 00 35.0   23.8r 04DG64    T09  C~89TZ      
2016 04  08.52637  12 15 12.26   +00 00 35.1   23.9r 04DG64    T09  C~89TZ      
2016 04  15.37454  12 14 43.41   +00 03 32.3   23.0y 04DG64    T09  C~89TZ      
2016 04  15.41093  12 14 43.26   +00 03 33.0   23.2y 04DG64    T09  C~89Ta      
2016 04  15.43491  12 14 43.15   +00 03 34.0   23.1y 04DG64    T09  C~89Ta      
2016 04  15.45396  12 14 43.07   +00 03 34.4   23.2y 04DG64    T09  C~89Ta      
2016 04  15.45934  12 14 43.05   +00 03 34.7   23.0y 04DG64    T09  C~89Ta      
2017 01  26.62279  12 24 35.78   -01 04 38.2   23.6z 04DG64    T09  C~89L7      
2017 01  26.63421  12 24 35.76   -01 04 37.8   23.5z 04DG64    T09  C~89L7      
2017 01  26.64766  12 24 35.73   -01 04 37.8   23.4z 04DG64    T09  C~89L7      
2017 01  26.65034  12 24 35.73   -01 04 37.7   23.6z 04DG64    T09  C~89L7      
2017 02  23.595374 12 23 16.62   -00 55 38.5         04DG64    T09  C~89L7      
2018 05  11.041655 12 23 00.768  -00 59 17.77  23.8V 04DG64    W84  C~8Gic      
2018 05  12.021227 12 22 57.864  -00 59 01.18  23.1V 04DG64    W84  C~8Gic      

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     0.06       0.00    -0.06
     2   0.0002      0.00    -0.09       0.00     0.08
     3   0.1638      0.00    -0.02       0.00    -0.09
     4   0.1639      0.00     0.03       0.00     0.15
     5   0.1747      0.00    -0.04       0.00     0.04
     6   0.1749      0.00     0.17       0.00     0.12
     7   0.1773      0.00    -0.10       0.00    -0.14
     8   0.2236      0.00    -0.08       0.00    -0.23
     9   0.2238      0.00    -0.01       0.00     0.18
    10   9.3814      0.00    -0.25       0.00     0.02
    11  10.3256      0.00     0.06       0.00    -0.08
    12  10.3256      0.00     0.08       0.00    -0.07
    13  10.3257      0.00     0.08       0.00    -0.05
    14  10.3257      0.00     0.06       0.00    -0.09
    15  10.3257      0.00     0.15       0.00     0.10
    16  10.3257      0.00     0.06       0.00    -0.07
    17  10.3257      0.00     0.09       0.00    -0.06
    18  11.2359      0.00     0.05       0.00    -0.02
    19  11.2360      0.00     0.01       0.00    -0.03
    20  12.2734      0.00    -0.21       0.00     0.22
    21  12.2734      0.00     0.03       0.00     0.24
    22  12.2735      0.00    -0.10       0.00     0.06
    23  12.2736      0.00    -0.10       0.00     0.09
    24  12.2736      0.00    -0.07       0.00     0.01
    25  12.2736      0.00    -0.09       0.00     0.11
    26  12.2737      0.00     0.04       0.00     0.11
    27  12.2737      0.00    -0.01       0.00     0.01
    28  12.2787      0.00     0.04       0.00     0.05
    29  12.2788      0.00     0.01       0.00    -0.10
    30  12.2788      0.00     0.00       0.00     0.04
    31  12.2789      0.00    -0.20       0.00     0.08
    32  12.2789      0.00     0.09       0.00     0.10
    33  12.2817      0.00     0.14       0.00    -0.07
    34  12.2820      0.00     0.05       0.00    -0.08
    35  12.2901      0.00    -0.02       0.00     0.03
    36  12.2901      0.00    -0.00       0.00    -0.05
    37  12.2901      0.00    -0.19       0.00    -0.02
    38  12.2902      0.00    -0.07       0.00     0.01
    39  12.2902      0.00     0.07       0.00     0.05
    40  12.3089      0.00    -0.02       0.00    -0.11
    41  12.3090      0.00     0.02       0.00    -0.32
    42  12.3091      0.00    -0.13       0.00     0.08
    43  12.3091      0.00    -0.13       0.00     0.00
    44  12.3091      0.00    -0.09       0.00     0.17
    45  13.0926      0.00     0.01       0.00    -0.11
    46  13.0926      0.00     0.03       0.00     0.14
    47  13.0927      0.00    -0.04       0.00    -0.04
    48  13.0927      0.00     0.04       0.00     0.03
    49  13.1692      0.00     0.05       0.00    -0.16
    50  14.3778      0.00     0.10       0.00    -0.05
    51  14.3805      0.00     0.09       0.00    -0.06

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.

04DG64    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        43.084    43.084    43.084
ecceobj         0.027     0.027     0.027
incobj          3.057     3.057     3.057
qmin           40.818    40.817    40.821
qmax           45.988    45.981    45.992
amean          43.279    43.279    43.279
amin           42.950    42.950    42.950
amax           43.632    43.630    43.633
emean           0.035     0.035     0.035
emin            0.015     0.015     0.015
emax            0.054     0.054     0.054
imean           2.398     2.398     2.398
imin            1.513     1.513     1.513
imax            3.166     3.166     3.166
excite_mean     0.055     0.055     0.055
fracstop        1.000     1.000     1.000
cjmean          3.089     3.089     3.089

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       170.7     170.8     170.7
kozaiamp        179.9     179.9     179.9