Orbit Fit and Astrometric record for 15FT561

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: 15FT561   
# Created Mon Jul  7 01:10:32 2025
# Orbit generated from Bernstein formalism
# Fitting     21 observations of     21
# Arc:   1.06y
# First observation: 2015/03/18
#  Last observation: 2016/04/08
Preliminary a, adot, b, bdot, g, gdot:
   0.000001   0.022348   0.000000   0.000364   0.023458   0.000000
# Chi-squared of fit:     6.30 DOF:     36 RMS:  0.10
# Min/Max residuals:    -0.22    0.27
# Exact a, adot, b, bdot, g, gdot:
  1.475030E-05  2.237663E-02  4.627993E-07  3.650677E-04  2.344924E-02  1.638515E-03
# Covariance matrix:
  3.3678E-13  2.3990E-12 -6.5799E-16  4.7232E-14  2.5347E-12  1.2173E-10
  2.3990E-12  8.5902E-11 -2.5531E-14  1.8142E-12  4.1643E-11  4.6737E-09
 -6.5799E-16 -2.5531E-14  1.3736E-13 -1.3344E-13 -1.1401E-14 -1.4061E-12
  4.7232E-14  1.8142E-12 -1.3344E-13  3.0128E-13  8.1514E-13  9.9853E-11
  2.5347E-12  4.1643E-11 -1.1401E-14  8.1514E-13  3.3890E-11  2.1005E-09
  1.2173E-10  4.6737E-09 -1.4061E-12  9.9853E-11  2.1005E-09  2.5724E-07
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.050725 -177.687711    0.085950   -0.000746   -0.988422  2457099.969108
# Heliocentric elements and errors
Epoch:              2457090.5000  =  2015/03/09
Mean Anomaly:           72.75461 +/-     0.537
Argument of Peri:      275.85874 +/-     2.455
Long of Asc Node:      185.23341 +/-     0.003
Inclination:             0.93567 +/-     0.001
Eccentricity:         0.07419526 +/-    0.0227
Semi-Major Axis:     44.38174699 +/-    0.1619
Time of Perihelion: 2435265.0599 +/-     107.9
Perihelion:          41.08883175 +/-    1.0164
Aphelion:            47.67466222 +/-    1.0202
Period (y)              295.6751 +/-      1.62
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -43.60475240 +/-    0.0106
Ecliptic Y           -1.67476411 +/-    0.0004
Ecliptic Z           -0.03771963 +/-    0.0000
Ecliptic XDOT        -0.00008920 +/-    0.0001
Ecliptic YDOT        -0.00262398 +/-    0.0000
Ecliptic ZDOT         0.00004254 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   43.63691888 +/-    0.0106
Geocenter to KBO     42.64530869 +/-    0.0106
# Hcoef:  8.53

The following table shows the complete astrometric record for 15FT561. 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 (15FT561) followed by the observatory code and reference code for the source of the astrometry.

2015 03  18.46833  12 08 24.36   -00 57 58.0   24.9r 15FT561   T09  C~8vFX      
2015 03  18.50341  12 08 24.20   -00 57 57.0   24.5r 15FT561   T09  C~8vFX      
2015 03  18.56444  12 08 23.94   -00 57 55.3   24.6r 15FT561   T09  C~8vFX      
2015 03  20.45524  12 08 15.78   -00 57 01.9   24.2i 15FT561   T09  C~8vFX      
2015 03  20.49422  12 08 15.60   -00 57 00.5   24.1i 15FT561   T09  C~8vFX      
2015 03  25.44596  12 07 54.19   -00 54 40.4   25.0g 15FT561   T09  C~8vFX      
2015 03  25.51107  12 07 53.89   -00 54 38.4   25.6g 15FT561   T09  C~8vFX      
2015 03  29.24886  12 07 37.79   -00 52 52.9   24.7y 15FT561   T09  C~8vFX      
2015 03  29.29096  12 07 37.61   -00 52 51.8   24.1y 15FT561   T09  C~8vFX      
2015 03  29.33172  12 07 37.44   -00 52 50.5   23.9y 15FT561   T09  C~8vFX      
2015 03  29.35353  12 07 37.34   -00 52 50.0   24.3y 15FT561   T09  C~8vFX      
2016 04  02.37629  12 12 01.67   -01 20 03.8   24.6i 15FT561   T09  C~8vFX      
2016 04  02.40651  12 12 01.55   -01 20 02.6   24.4i 15FT561   T09  C~8vFX      
2016 04  02.43106  12 12 01.44   -01 20 02.1   24.3i 15FT561   T09  C~8vFX      
2016 04  02.45551  12 12 01.34   -01 20 01.5   24.3i 15FT561   T09  C~8vFX      
2016 04  02.48014  12 12 01.23   -01 20 00.8   24.4i 15FT561   T09  C~8vFX      
2016 04  02.50441  12 12 01.13   -01 20 00.1   24.6i 15FT561   T09  C~8vFX      
2016 04  08.50164  12 11 35.98   -01 17 15.7   26.1r 15FT561   T09  C~8vFX      
2016 04  08.50945  12 11 35.94   -01 17 15.3   25.6r 15FT561   T09  C~8vFX      
2016 04  08.51580  12 11 35.90   -01 17 15.3   25.3r 15FT561   T09  C~8vFX      
2016 04  08.52214  12 11 35.88   -01 17 15.0   26.0r 15FT561   T09  C~8vFX      

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     0.07       0.00    -0.04
     2   0.0001     -2.60    -0.02      -0.04    -0.07
     3   0.0003     -6.85     0.09      -0.03    -0.05
     4   0.0054   -140.38     0.04       0.32    -0.11
     5   0.0055   -143.41    -0.19       0.54     0.11
     6   0.0191   -493.75     0.09       1.44     0.01
     7   0.0193   -498.68    -0.16       1.49     0.08
     8   0.0295   -762.19    -0.06       2.29     0.00
     9   0.0296   -765.10     0.02       2.23    -0.06
    10   0.0297   -767.96     0.06       2.41     0.13
    11   0.0298   -769.53     0.05       2.27    -0.00
    12   1.0429   3517.81    -0.07      78.41    -0.13
    13   1.0430   3515.68    -0.06      78.79     0.27
    14   1.0430   3513.97    -0.04      78.60     0.08
    15   1.0431   3512.35     0.07      78.55     0.04
    16   1.0432   3510.56     0.02      78.54     0.03
    17   1.0432   3508.91     0.08      78.59     0.08
    18   1.0596   3097.38     0.18      79.64    -0.11
    19   1.0597   3096.67     0.00      79.77     0.02
    20   1.0597   3096.12    -0.11      79.53    -0.22
    21   1.0597   3095.72    -0.07      79.69    -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.

15FT561    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        43.988    44.679    43.627
ecceobj         0.073     0.134     0.017
incobj          0.940     0.940     0.940
qmin           39.828    37.763    41.990
qmax           48.772    52.272    45.850
amean          44.177    44.853    43.825
amin           43.824    44.475    43.484
amax           44.562    45.282    44.167
emean           0.079     0.139     0.023
emin            0.063     0.123     0.006
emax            0.095     0.155     0.038
imean           2.030     2.057     2.121
imin            1.215     1.095     1.416
imax            2.752     2.880     2.768
excite_mean     0.087     0.144     0.044
fracstop        1.000     1.000     1.000
cjmean          3.095     3.086     3.097

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       204.1     195.5     201.2
kozaiamp        180.0     180.0     180.0