Orbit Fit and Astrometric record for 07CR79

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: 07CR79    
# Created Sun Nov 24 02:08:54 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     21 observations of     21
# Arc:  17.16y
# First observation: 2005/02/10
#  Last observation: 2022/04/08
# Chi-squared of fit:    14.53 DOF:     36 RMS:  0.15
# Min/Max residuals:    -0.19    0.40
# Exact a, adot, b, bdot, g, gdot:
  1.600288E-05  2.954512E-02  5.572872E-06  1.183567E-02  2.785925E-02  5.743752E-04
# Covariance matrix:
  2.0271E-13 -5.2403E-14  2.9664E-14 -1.8630E-14  7.5892E-14 -8.9376E-14
 -5.2403E-14  2.7682E-14 -1.7073E-14  1.0989E-14 -1.5451E-14  5.2007E-14
  2.9664E-14 -1.7073E-14  1.3380E-13 -1.7235E-14  1.7885E-14 -3.4919E-14
 -1.8630E-14  1.0989E-14 -1.7235E-14  6.5117E-15 -9.2985E-15  2.2304E-14
  7.5892E-14 -1.5451E-14  1.7885E-14 -9.2985E-15  2.5044E-13 -4.9781E-14
 -8.9376E-14  5.2007E-14 -3.4919E-14  2.2304E-14 -4.9781E-14  1.0600E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
    1.392795  136.524240   -0.084238    0.023932   -0.979635  2453411.809733
# Heliocentric elements and errors
Epoch:              2453412.5000  =  2005/02/11
Mean Anomaly:            3.57226 +/-     0.002
Argument of Peri:      357.87024 +/-     0.003
Long of Asc Node:      133.27406 +/-     0.000
Inclination:            21.83601 +/-     0.000
Eccentricity:         0.22421196 +/-    0.0001
Semi-Major Axis:     47.49145061 +/-    0.0051
Time of Perihelion: 2452226.2883 +/-       0.6
Perihelion:          36.84329936 +/-    0.0051
Aphelion:            58.13960186 +/-    0.0070
Period (y)              327.2890 +/-      0.05
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -26.81363137 +/-    0.0005
Ecliptic Y           25.30267818 +/-    0.0004
Ecliptic Z            0.87266594 +/-    0.0000
Ecliptic XDOT        -0.00201838 +/-    0.0000
Ecliptic YDOT        -0.00209480 +/-    0.0000
Ecliptic ZDOT         0.00116424 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   36.87759503 +/-    0.0005
Geocenter to KBO     35.89474555 +/-    0.0006
# Hcoef:  7.32

The following table shows the complete astrometric record for 07CR79. 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 (07CR79) followed by the observatory code and reference code for the source of the astrometry.

2005 02  10.30899  09 17 40.05   +17 12 43.5   23.4g 07CR79    568  C~0VEU      
2005 02  10.39196  09 17 39.59   +17 12 45.9   23.5g 07CR79    568  C~0VEU      
2005 02  10.43152  09 17 39.36   +17 12 47.3   23.4g 07CR79    568  C~0VEU      
2005 04  11.30482  09 13 43.08   +17 36 02.0   23.3i 07CR79    568  C~0VEU      
2005 04  11.33442  09 13 43.03   +17 36 02.4   23.3i 07CR79    568  C~0VEU      
2005 04  11.35929  09 13 42.99   +17 36 02.7   23.4i 07CR79    568  C~0VEU      
2007 02  14.45798  09 32 35.01   +17 28 40.4   23.0r 07CR79    568  C74770      
2007 02  14.49571  09 32 34.80   +17 28 41.6   23.0r 07CR79    568  C74770      
2007 02  14.52893  09 32 34.63   +17 28 42.7   23.0r 07CR79    568  C74770      
2007 02  15.47269  09 32 29.57   +17 29 13.3   23.1r 07CR79    568  C74770      
2007 11  08.51341  09 44 29.36   +16 55 10.2   22.0r 07CR79    695  C~0VEU      
2007 11  09.49094  09 44 31.29   +16 55 12.8   22.1r 07CR79    695  C~0VEU      
2008 05  04.16494  09 35 54.96   +17 59 00.0         07CR79    695  C~0VEU      
2008 05  05.13645  09 35 55.33   +17 58 59.5         07CR79    695  C~0VEU      
2008 05  05.13952  09 35 55.31   +17 58 59.2         07CR79    695  C~0VEU      
2015 02  18.26506  10 32 34.73   +17 44 04.9   22.3R 07CR79    695  C~1M6T      
2015 02  18.35525  10 32 34.26   +17 44 08.4         07CR79    695  C~1M6T      
2015 02  18.44818  10 32 33.78   +17 44 11.7         07CR79    695  C~1M6T      
2022 04  08.150950 11 19 33.080  +17 28 59.81  22.8G 07CR79    G37  C~5ZWP      
2022 04  08.185850 11 19 32.948  +17 29 00.49        07CR79    G37  C~5ZWP      
2022 04  08.220830 11 19 32.800  +17 29 01.01        07CR79    G37  C~5ZWP      

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     0.23       0.00     0.18
     2   0.0002      0.00     0.16       0.00    -0.04
     3   0.0003      0.00    -0.03       0.00     0.12
     4   0.1643      0.00    -0.14       0.00    -0.17
     5   0.1643      0.00    -0.16       0.00    -0.11
     6   0.1644      0.00    -0.15       0.00    -0.09
     7   2.0100      0.00    -0.06       0.00    -0.10
     8   2.0101      0.00    -0.12       0.00    -0.12
     9   2.0102      0.00     0.04       0.00    -0.09
    10   2.0128      0.00    -0.14       0.00     0.05
    11   2.7411      0.00     0.09       0.00     0.13
    12   2.7438      0.00     0.08       0.00     0.36
    13   3.2275      0.00    -0.19       0.00    -0.16
    14   3.2302      0.00     0.40       0.00     0.22
    15   3.2302      0.00     0.09       0.00    -0.07
    16  10.0204      0.00    -0.08       0.00    -0.10
    17  10.0207      0.00    -0.07       0.00     0.04
    18  10.0209      0.00    -0.01       0.00    -0.11
    19  17.1549      0.00    -0.17       0.00     0.11
    20  17.1550      0.00     0.10       0.00     0.07
    21  17.1551      0.00     0.14       0.00    -0.13

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.

07CR79    quality flag:3

Type:       SCATNEAR  SCATNEAR  SCATNEAR

axisobj        47.228    47.228    47.228
ecceobj         0.220     0.220     0.220
incobj         21.878    21.878    21.878
qmin           35.474    35.408    35.451
qmax           59.539    59.600    59.381
amean          47.191    47.192    47.192
amin           46.759    46.734    46.771
amax           47.753    47.782    47.732
emean           0.228     0.228     0.228
emin            0.210     0.210     0.210
emax            0.247     0.247     0.247
imean          20.240    20.241    20.238
imin           19.645    19.650    19.638
imax           20.758    20.756    20.764
excite_mean     0.414     0.414     0.415
fracstop        1.000     1.000     1.000
cjmean          2.926     2.926     2.926

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       168.6     168.4     168.8
kozaiamp        180.0     180.0     179.9