Orbit Fit and Astrometric record for 15FW562

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: 15FW562   
# Created Thu Jul  3 01:10:30 2025
# Orbit generated from Bernstein formalism
# Fitting      9 observations of      9
# Arc:   7.08d
# First observation: 2015/03/18
#  Last observation: 2015/03/25
# WARNING Fitting with energy constraint
# WARNING and with gdot fixed = 0
# Chi-squared of fit:     6.21 DOF:     14 RMS:  0.15
# Min/Max residuals:    -0.25    0.28
# Exact a, adot, b, bdot, g, gdot:
  1.369877E-05  2.111040E-02  2.589612E-07  8.428405E-06  2.243057E-02  0.000000E+00
# Covariance matrix:
  2.7739E-11  3.8786E-08  6.8222E-14 -1.2489E-12  6.1563E-09  0.0000E+00
  3.8786E-08  5.4825E-05  9.6390E-11 -1.7646E-09  8.6982E-06  0.0000E+00
  6.8222E-14  9.6390E-11  2.7611E-13 -1.6068E-11  1.5293E-11  0.0000E+00
 -1.2489E-12 -1.7646E-09 -1.6068E-11  2.2897E-09 -2.7997E-10  0.0000E+00
  6.1563E-09  8.6982E-06  1.5293E-11 -2.7997E-10  1.3801E-06  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  1.4851E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.917811  179.629975    0.039703   -0.015750   -0.991231  2457099.963238
# Heliocentric elements and errors
Epoch:              2457090.5000  =  2015/03/09
Mean Anomaly:            0.87492 +/-    99.091
Argument of Peri:      270.65211 +/-   166.285
Long of Asc Node:      267.97306 +/-     8.319
Inclination:             0.89811 +/-     0.004
Eccentricity:         0.02721516 +/-    0.5590
Semi-Major Axis:     46.85128387 +/-   24.5220
Time of Perihelion: 2456805.8267 +/-  383641.4
Perihelion:          45.57621850 +/-   35.4259
Aphelion:            48.12634924 +/-   36.3380
Period (y)              320.6937 +/-    251.78
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -45.56956904 +/-    2.3346
Ecliptic Y            0.33380633 +/-    0.0153
Ecliptic Z           -0.71409463 +/-    0.0374
Ecliptic XDOT        -0.00002007 +/-    0.0015
Ecliptic YDOT        -0.00258243 +/-    0.0008
Ecliptic ZDOT         0.00000112 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   45.57638621 +/-    2.3342
Geocenter to KBO     44.58201138 +/-    2.3349
# Hcoef:  8.97

The following table shows the complete astrometric record for 15FW562. 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 (15FW562) followed by the observatory code and reference code for the source of the astrometry.

2015 03  18.46246  11 57 10.90   -00 41 41.6   25.2r 15FW562   T09  C~8vFZ      
2015 03  18.49910  11 57 10.71   -00 41 40.6   25.3r 15FW562   T09  C~8vFZ      
2015 03  18.53831  11 57 10.58   -00 41 39.2   25.0r 15FW562   T09  C~8vFZ      
2015 03  18.56877  11 57 10.43   -00 41 38.5   25.1r 15FW562   T09  C~8vFZ      
2015 03  20.44977  11 57 02.62   -00 40 47.8   25.2i 15FW562   T09  C~8vFZ      
2015 03  20.48863  11 57 02.46   -00 40 46.8   25.2i 15FW562   T09  C~8vFZ      
2015 03  25.47635  11 56 41.74   -00 38 32.1   26.5g 15FW562   T09  C~8vFZ      
2015 03  25.51534  11 56 41.59   -00 38 30.7   26.3g 15FW562   T09  C~8vFZ      
2015 03  25.54542  11 56 41.45   -00 38 30.0   25.9g 15FW562   T09  C~8vFZ      

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     0.24       0.00    -0.05
     2   0.0001     -3.01    -0.24      -0.22    -0.25
     3   0.0002     -5.36     0.11       0.29     0.28
     4   0.0003     -7.70    -0.13       0.04     0.04
     5   0.0054   -135.34    -0.03      -0.04     0.00
     6   0.0055   -137.94     0.05      -0.08    -0.02
     7   0.0192   -476.66     0.01      -0.13    -0.21
     8   0.0193   -479.28     0.07       0.26     0.20
     9   0.0194   -481.49    -0.08       0.07     0.01

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.