Orbit Fit and Astrometric record for 17CV56

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: 17CV56    
# Created Wed Mar 26 01:11:06 2025
# Orbit generated from Bernstein formalism
# Fitting     22 observations of     22
# Arc:   1.87y
# First observation: 2015/03/22
#  Last observation: 2017/02/01
Preliminary a, adot, b, bdot, g, gdot:
   0.000045   0.019511   0.000012   0.003854   0.021072   0.000000
# Chi-squared of fit:     5.95 DOF:     38 RMS:  0.09
# Min/Max residuals:    -0.19    0.18
# Exact a, adot, b, bdot, g, gdot:
  1.337199E-05  1.912478E-02  2.621343E-06  3.868047E-03  2.190375E-02  9.909844E-04
# Covariance matrix:
  2.9253E-13 -2.9607E-13  5.5037E-15 -2.7603E-14 -1.3154E-13 -3.6745E-12
 -2.9607E-13  3.2372E-12 -1.0335E-14  4.1208E-13  4.1927E-13  5.5153E-11
  5.5037E-15 -1.0335E-14  2.5366E-13 -1.4993E-13 -1.8541E-14 -3.4344E-13
 -2.7603E-14  4.1208E-13 -1.4993E-13  1.7345E-13  8.2621E-14  7.5395E-12
 -1.3154E-13  4.1927E-13 -1.8541E-14  8.2621E-14  4.3816E-13  1.0990E-11
 -3.6745E-12  5.5153E-11 -3.4344E-13  7.5395E-12  1.0990E-11  1.0085E-09
#      lat0       lon0       xBary       yBary       zBary        JD0
  -14.134468  140.607192   -0.646789   -0.183949   -0.731013  2457103.877264
# Heliocentric elements and errors
Epoch:              2457100.5000  =  2015/03/19
Mean Anomaly:          129.27417 +/-     0.772
Argument of Peri:      172.49678 +/-     0.755
Long of Asc Node:      190.94043 +/-     0.003
Inclination:            18.03167 +/-     0.001
Eccentricity:         0.08819776 +/-    0.0010
Semi-Major Axis:     43.76136454 +/-    0.0121
Time of Perihelion: 2419130.2061 +/-     226.2
Perihelion:          39.90171007 +/-    0.0448
Aphelion:            47.62101902 +/-    0.0453
Period (y)              289.4973 +/-      0.12
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -35.21064885 +/-    0.0010
Ecliptic Y           28.07506995 +/-    0.0008
Ecliptic Z          -11.14857684 +/-    0.0003
Ecliptic XDOT        -0.00170454 +/-    0.0000
Ecliptic YDOT        -0.00170204 +/-    0.0000
Ecliptic ZDOT         0.00043869 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   46.39278080 +/-    0.0009
Geocenter to KBO     45.65428897 +/-    0.0014
# Hcoef:  7.85

The following table shows the complete astrometric record for 17CV56. 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 (17CV56) followed by the observatory code and reference code for the source of the astrometry.

2015 03  22.376486 09 14 12.92   +01 11 20.8         17CV56    T09  C~83Ey      
2015 03  22.40027  09 14 12.84   +01 11 21.3   24.5i 17CV56    T09  C~8ifR      
2015 03  22.41123  09 14 12.81   +01 11 22.0   24.1i 17CV56    T09  C~8ifR      
2015 03  22.42769  09 14 12.76   +01 11 22.2   24.0i 17CV56    T09  C~8ifR      
2015 03  22.438718 09 14 12.74   +01 11 22.6         17CV56    T09  C~83Ey      
2015 11  10.586966 09 24 59.22   +00 43 09.2         17CV56    T09  C~83Ey      
2015 11  10.637751 09 24 59.26   +00 43 08.1         17CV56    T09  C~83Ey      
2016 11  28.52476  09 29 21.22   +00 30 23.4   24.8r 17CV56    T09  C~83Ey      
2016 11  28.56332  09 29 21.17   +00 30 22.9   24.8r 17CV56    T09  C~83Ey      
2016 11  28.58020  09 29 21.15   +00 30 22.7   24.7r 17CV56    T09  C~83Ey      
2016 11  28.61822  09 29 21.13   +00 30 22.2   24.7r 17CV56    T09  C~83Ey      
2016 11  29.50691  09 29 20.44   +00 30 11.1   24.3i 17CV56    T09  C~83Ey      
2016 11  29.62736  09 29 20.35   +00 30 09.7   24.7z 17CV56    T09  C~83Ey      
2016 11  29.63007  09 29 20.34   +00 30 09.7   24.2z 17CV56    T09  C~83Ey      
2016 11  29.65490  09 29 20.33   +00 30 09.4   24.0z 17CV56    T09  C~83Ey      
2017 01  02.418269 09 28 09.38   +00 28 17.0         17CV56    T09  C~83Ey      
2017 01  02.420936 09 28 09.37   +00 28 16.9         17CV56    T09  C~83Ey      
2017 02  01.49516  09 26 13.75   +00 34 53.2   23.9i 17CV56    T09  C~83Ey      
2017 02  01.50344  09 26 13.71   +00 34 53.4   24.8i 17CV56    T09  C~83Ey      
2017 02  01.53643  09 26 13.58   +00 34 54.0   24.2i 17CV56    T09  C~83Ey      
2017 02  01.54461  09 26 13.53   +00 34 54.2   24.1i 17CV56    T09  C~83Ey      
2017 02  01.55276  09 26 13.49   +00 34 54.2   24.1i 17CV56    T09  C~83Ey      

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     0.04
     2   0.0001     -1.30    -0.01       0.11    -0.19
     3   0.0001     -1.94    -0.11       0.63     0.18
     4   0.0001     -2.71    -0.06       0.59    -0.09
     5   0.0002     -3.12     0.09       0.88     0.04
     6   0.6385   9750.50    -0.05    1375.90     0.03
     7   0.6386   9751.41     0.05    1375.04     0.00
     8   1.6897  13738.18     0.18    1860.74     0.08
     9   1.6898  13737.61    -0.09    1860.03    -0.03
    10   1.6898  13737.39    -0.19    1859.74    -0.04
    11   1.6899  13737.26    -0.03    1859.18    -0.01
    12   1.6923  13730.80    -0.13    1845.39    -0.14
    13   1.6927  13729.95     0.08    1843.64    -0.00
    14   1.6927  13729.80    -0.04    1843.59    -0.01
    15   1.6928  13729.75     0.14    1843.26     0.05
    16   1.7852  12747.89     0.05    1407.01     0.14
    17   1.7852  12747.78     0.07    1406.87     0.03
    18   1.8675  10969.91     0.02    1248.64     0.02
    19   1.8676  10969.27    -0.05    1248.65     0.04
    20   1.8677  10967.23     0.15    1248.62     0.04
    21   1.8677  10966.45    -0.08    1248.58     0.00
    22   1.8677  10965.88    -0.10    1248.39    -0.18

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.

17CV56    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        43.599    43.638    43.561
ecceobj         0.095     0.097     0.093
incobj         18.076    18.075    18.078
qmin           38.494    38.271    38.632
qmax           48.907    49.172    48.717
amean          43.571    43.612    43.533
amin           43.229    43.276    43.188
amax           43.951    43.992    43.904
emean           0.098     0.103     0.095
emin            0.086     0.087     0.082
emax            0.113     0.119     0.110
imean          18.230    18.214    18.240
imin           17.835    17.717    17.847
imax           18.568    18.660    18.606
excite_mean     0.328     0.329     0.327
fracstop        1.000     1.000     1.000
cjmean          2.965     2.964     2.965

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       182.1     186.0     181.1
kozaiamp        180.0     179.9     179.9