Orbit Fit and Astrometric record for 15FU561

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: 15FU561   
# Created Mon Jul  7 01:10:32 2025
# Orbit generated from Bernstein formalism
# Fitting     20 observations of     20
# Arc:  10.88d
# First observation: 2015/03/18
#  Last observation: 2015/03/29
Preliminary a, adot, b, bdot, g, gdot:
   0.000000   0.031916  -0.000000  -0.011935   0.027857   0.000000
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# WARNING Fitting with energy constraint
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# Chi-squared of fit:     5.51 DOF:     35 RMS:  0.09
# Min/Max residuals:    -0.17    0.21
# Exact a, adot, b, bdot, g, gdot:
  1.407478E-05  2.332459E-02 -7.217370E-06 -1.193427E-02  2.648732E-02 -9.064869E-03
# Covariance matrix:
  4.3578E-11  7.0847E-08 -1.9654E-13  4.2629E-12  1.1281E-08  3.0264E-08
  7.0847E-08  1.1581E-04 -3.2570E-10  8.6089E-09  1.8435E-05  4.4904E-05
 -1.9654E-13 -3.2570E-10  1.8846E-13 -7.9420E-12 -5.1715E-11  6.7890E-11
  4.2629E-12  8.6089E-09 -7.9420E-12  5.6695E-10  1.3217E-09 -6.8038E-08
  1.1281E-08  1.8435E-05 -5.1715E-11  1.3217E-09  2.9348E-06  7.2837E-06
  3.0264E-08  4.4904E-05  6.7890E-11 -6.8038E-08  7.2837E-06  2.1567E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
    0.793267 -179.023159    0.062789    0.013837   -0.990068  2457099.974968
# Heliocentric elements and errors
Epoch:              2457090.5000  =  2015/03/09
Mean Anomaly:          302.10245 +/-    64.046
Argument of Peri:      274.62776 +/-    87.618
Long of Asc Node:        2.39589 +/-     0.689
Inclination:            27.07117 +/-    10.700
Eccentricity:         0.33476495 +/-    0.5357
Semi-Major Axis:     42.02800194 +/-   22.2656
Time of Perihelion: 2473095.8153 +/-   12316.3
Perihelion:          27.95850016 +/-   26.9508
Aphelion:            56.09750373 +/-   37.2853
Period (y)              272.4685 +/-    216.52
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -38.73901671 +/-    2.4412
Ecliptic Y           -0.59777497 +/-    0.0414
Ecliptic Z            0.52243424 +/-    0.0338
Ecliptic XDOT         0.00095737 +/-    0.0015
Ecliptic YDOT        -0.00240068 +/-    0.0010
Ecliptic ZDOT        -0.00124635 +/-    0.0001
# Distances at JD0 (AU)
Heliocenter to KBO   38.74715071 +/-    2.4407
Geocenter to KBO     37.75391153 +/-    2.4418
# Hcoef:  7.26

The following table shows the complete astrometric record for 15FU561. 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 (15FU561) followed by the observatory code and reference code for the source of the astrometry.

2015 03  18.47419  12 04 50.82   +00 20 21.4   23.0r 15FU561   T09  C~8vFX      
2015 03  18.50772  12 04 50.64   +00 20 22.2   23.0r 15FU561   T09  C~8vFX      
2015 03  18.55140  12 04 50.42   +00 20 23.4   23.1r 15FU561   T09  C~8vFX      
2015 03  18.57737  12 04 50.28   +00 20 24.1   23.0r 15FU561   T09  C~8vFX      
2015 03  20.41961  12 04 40.83   +00 21 12.1   22.8i 15FU561   T09  C~8vFX      
2015 03  20.46072  12 04 40.63   +00 21 13.3   22.8i 15FU561   T09  C~8vFX      
2015 03  20.46343  12 04 40.60   +00 21 13.3   22.9i 15FU561   T09  C~8vFX      
2015 03  20.49965  12 04 40.43   +00 21 14.2   22.6i 15FU561   T09  C~8vFX      
2015 03  20.55748  12 04 40.12   +00 21 15.8   22.8i 15FU561   T09  C~8vFX      
2015 03  25.45174  12 04 14.95   +00 23 23.5   23.5g 15FU561   T09  C~8vFX      
2015 03  25.46918  12 04 14.87   +00 23 24.0   23.5g 15FU561   T09  C~8vFX      
2015 03  25.48492  12 04 14.78   +00 23 24.4   23.5g 15FU561   T09  C~8vFX      
2015 03  25.51323  12 04 14.64   +00 23 25.0   23.5g 15FU561   T09  C~8vFX      
2015 03  25.55400  12 04 14.43   +00 23 26.2   23.4g 15FU561   T09  C~8vFX      
2015 03  29.25584  12 03 55.50   +00 25 01.6   23.2y 15FU561   T09  C~8vFX      
2015 03  29.29637  12 03 55.30   +00 25 02.6   22.8y 15FU561   T09  C~8vFX      
2015 03  29.31534  12 03 55.18   +00 25 03.3   22.6y 15FU561   T09  C~8vFX      
2015 03  29.32352  12 03 55.14   +00 25 03.3   22.6y 15FU561   T09  C~8vFX      
2015 03  29.33991  12 03 55.07   +00 25 04.0   22.7y 15FU561   T09  C~8vFX      
2015 03  29.35897  12 03 54.96   +00 25 04.3   22.8y 15FU561   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    -0.03       0.00     0.02
     2   0.0001     -2.80    -0.07      -0.34    -0.08
     3   0.0002     -6.30     0.01      -0.55     0.02
     4   0.0003     -8.51    -0.07      -0.74     0.01
     5   0.0053   -157.65    -0.05     -13.08    -0.12
     6   0.0054   -160.88     0.11     -13.17     0.08
     7   0.0054   -161.29    -0.08     -13.35    -0.08
     8   0.0055   -163.99     0.21     -13.54    -0.00
     9   0.0057   -168.89     0.06     -13.92     0.03
    10   0.0191   -566.08    -0.13     -46.91     0.01
    11   0.0192   -567.38     0.00     -46.93     0.12
    12   0.0192   -568.78    -0.10     -47.10     0.07
    13   0.0193   -570.94     0.06     -47.38    -0.01
    14   0.0194   -574.31     0.03     -47.54     0.13
    15   0.0295   -872.78     0.07     -72.93    -0.07
    16   0.0296   -875.93     0.21     -73.21    -0.06
    17   0.0297   -877.86    -0.17     -73.28     0.01
    18   0.0297   -878.41    -0.06     -73.52    -0.17
    19   0.0297   -879.65     0.03     -73.29     0.17
    20   0.0298   -881.28    -0.05     -73.67    -0.07

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.

15FU561    quality flag:0

Type:      ERR2LARGE ERR2LARGE ERR2LARGE

axisobj         0.000     0.000     0.000
ecceobj        -1.000    -1.000    -1.000
incobj         -1.000    -1.000    -1.000
qmin            0.000     0.000     0.000
qmax            0.000     0.000     0.000
amean           0.000     0.000     0.000
amin            0.000     0.000     0.000
amax            0.000     0.000     0.000
emean           0.000     0.000     0.000
emin            0.000     0.000     0.000
emax            0.000     0.000     0.000
imean           0.000     0.000     0.000
imin            0.000     0.000     0.000
imax            0.000     0.000     0.000
excite_mean     0.000     0.000     0.000
fracstop        0.000     0.000     0.000
cjmean          0.000     0.000     0.000

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         0.0       0.0       0.0
kozaiamp          0.0       0.0       0.0