Orbit Fit and Astrometric record for 17CF60

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: 17CF60    
# Created Tue Jan 21 02:11:10 2025
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     19 observations of     22
# Arc:   2.32y
# First observation: 2016/02/12
#  Last observation: 2018/06/10
# Chi-squared of fit:    13.54 DOF:     32 RMS:  0.15
# Min/Max residuals:    -0.21    0.32
# Exact a, adot, b, bdot, g, gdot:
  1.310797E-05  1.831079E-02 -1.118898E-06 -1.141793E-03  2.123703E-02 -7.619621E-04
# Covariance matrix:
  3.4281E-13 -3.1571E-13 -6.2968E-15  1.7709E-14 -2.6260E-13 -1.6524E-12
 -3.1571E-13  3.8089E-13  8.8730E-15 -2.1676E-14  2.8751E-13  2.0489E-12
 -6.2968E-15  8.8730E-15  1.0120E-13 -1.7171E-14 -4.7122E-15  4.5692E-14
  1.7709E-14 -2.1676E-14 -1.7171E-14  9.6089E-15 -2.1198E-14 -1.2040E-13
 -2.6260E-13  2.8751E-13 -4.7122E-15 -2.1198E-14  6.7055E-13  1.7014E-12
 -1.6524E-12  2.0489E-12  4.5692E-14 -1.2040E-13  1.7014E-12  1.1299E-11
#      lat0       lon0       xBary       yBary       zBary        JD0
  -12.489340  144.397294    0.030701   -0.212767   -0.961410  2457430.845210
# Heliocentric elements and errors
Epoch:              2457430.5000  =  2016/02/12
Mean Anomaly:          209.55543 +/-     0.100
Argument of Peri:       49.30184 +/-     0.094
Long of Asc Node:      250.78853 +/-     0.001
Inclination:            12.73877 +/-     0.000
Eccentricity:         0.09584321 +/-    0.0001
Semi-Major Axis:     44.27266894 +/-    0.0052
Time of Perihelion: 2502395.6438 +/-      31.8
Perihelion:          40.02943408 +/-    0.0065
Aphelion:            48.51590379 +/-    0.0072
Period (y)              294.5858 +/-      0.05
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -38.16651334 +/-    0.0015
Ecliptic Y           27.35987567 +/-    0.0010
Ecliptic Z          -10.18313186 +/-    0.0004
Ecliptic XDOT        -0.00127078 +/-    0.0000
Ecliptic YDOT        -0.00200069 +/-    0.0000
Ecliptic ZDOT        -0.00012246 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   48.05147675 +/-    0.0013
Geocenter to KBO     47.08763095 +/-    0.0018
# Hcoef:  7.03

The following table shows the complete astrometric record for 17CF60. 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 (17CF60) followed by the observatory code and reference code for the source of the astrometry.

2016 02  12.344421 09 30 17.72   +01 35 09.7         17CF60    T09  C~89UW      
2016 02  12.37560  09 30 17.58   +01 35 10.1   23.4y 17CF60    T09  C~8COt      
2016 02  12.41099  09 30 17.44   +01 35 11.0   23.3y 17CF60    T09  C~8COt      
2016 02  12.443814 09 30 17.31   +01 35 11.6         17CF60    T09  C~89UW      
2016 12  25.483314 09 37 07.41   +01 02 29.4         17CF60    T09  C~89UW      
2017 01  21.37198  09 35 38.47   +01 05 09.2   24.0z 17CF60    T09  C~89UW      
2017 01  21.39613  09 35 38.37   +01 05 09.4   23.4z 17CF60    T09  C~89UW      
2017 01  21.41490  09 35 38.28   +01 05 09.5   23.5z 17CF60    T09  C~89UW      
2017 01  28.391375 09 35 10.54   +01 06 45.5         17CF60    T09  C~89UW      
2017 01  28.399817 09 35 10.50   +01 06 45.7         17CF60    T09  C~89UW      
2017 02  01.48142  09 34 53.77   +01 07 51.3   23.6i 17CF60    T09  C~89UW      
2017 02  01.48410  09 34 53.76   +01 07 51.2   23.6i 17CF60    T09  C~89UW      
2017 02  01.51446  09 34 53.63   +01 07 51.7   23.8i 17CF60    T09  C~89UW      
2017 02  01.52270  09 34 53.59   +01 07 51.7   23.5i 17CF60    T09  C~89UW      
2017 02  01.52538  09 34 53.59   +01 07 52.0   23.4i 17CF60    T09  C~89UW      
2017 02  01.55545  09 34 53.44   +01 07 52.2   23.7i 17CF60    T09  C~89UW      
2017 03  04.385780 09 32 47.36   +01 18 47.7         17CF60    T09  C~89UW      
2018 06  10.248590 09 35 18.52   +01 22 51.4         17CF60    T14  C~89UW      
2018 06  10.251851 09 35 18.53   +01 22 51.5         17CF60    T14  C~89UW      
2024 12  31.41651  10 07 56.604  -02 10 38.13  23.9G 17CF60    G37              
2024 12  31.46879  10 07 56.473  -02 10 38.16        17CF60    G37              
2024 12  31.52114  10 07 56.338  -02 10 38.33        17CF60    G37              

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     0.12       0.00     0.02
     2   0.0001      0.00     0.01       0.00    -0.21
     3   0.0002      0.00     0.17       0.00    -0.02
     4   0.0003      0.00     0.32       0.00    -0.08
     5   0.8683      0.00     0.16       0.00    -0.03
     6   0.9419      0.00     0.32       0.00     0.11
     7   0.9420      0.00     0.24       0.00     0.02
     8   0.9420      0.00     0.00       0.00    -0.11
     9   0.9611      0.00     0.23       0.00    -0.21
    10   0.9611      0.00     0.16       0.00    -0.14
    11   0.9723      0.00     0.17       0.00     0.13
    12   0.9723      0.00     0.18       0.00    -0.01
    13   0.9724      0.00     0.15       0.00    -0.02
    14   0.9724      0.00     0.07       0.00    -0.16
    15   0.9724      0.00     0.24       0.00     0.10
    16   0.9725      0.00    -0.12       0.00    -0.21
    17   1.0569      0.00     0.11       0.00    -0.13
    18   2.3242      0.00     0.14       0.00    -0.12
    19   2.3242      0.00     0.16       0.00    -0.02
    20   8.8845      0.00 (   6.07)      0.00 (  -4.06)
    21   8.8847      0.00 (   6.07)      0.00 (  -4.03)
    22   8.8848      0.00 (   6.01)      0.00 (  -4.15)

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.

17CF60    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        44.057    44.057    44.057
ecceobj         0.100     0.100     0.100
incobj         12.716    12.716    12.716
qmin           38.967    38.967    38.967
qmax           49.458    49.462    49.455
amean          44.084    44.084    44.084
amin           43.718    43.718    43.719
amax           44.472    44.472    44.473
emean           0.100     0.100     0.100
emin            0.087     0.087     0.087
emax            0.113     0.113     0.113
imean          14.325    14.325    14.325
imin           13.803    13.803    13.803
imax           14.763    14.763    14.763
excite_mean     0.267     0.267     0.267
fracstop        1.000     1.000     1.000
cjmean          3.015     3.015     3.015

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       177.9     177.9     177.9
kozaiamp        180.0     180.0     180.0