Orbit Fit and Astrometric record for 15FF490

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: 15FF490   
# Created Sun Feb 23 02:10:20 2025
# Orbit generated from Bernstein formalism
# Fitting     20 observations of     20
# Arc:  65.88d
# First observation: 2015/03/18
#  Last observation: 2015/05/23
Preliminary a, adot, b, bdot, g, gdot:
  -0.000000   0.040769   0.000001   0.004893   0.030632   0.000000
# WARNING Fitting with energy constraint
# Chi-squared of fit:     5.88 DOF:     35 RMS:  0.10
# Min/Max residuals:    -0.23    0.19
# Exact a, adot, b, bdot, g, gdot:
  1.659444E-05  3.075402E-02  2.577395E-06  4.953851E-03  2.904188E-02 -1.913820E-03
# Covariance matrix:
  1.1194E-12  1.8975E-09  1.5554E-13 -1.3864E-11  2.9033E-10 -1.8602E-08
  1.8975E-09  4.0494E-06  3.3994E-10 -3.0281E-08  6.1596E-07 -4.0441E-05
  1.5554E-13  3.3994E-10  1.3876E-13 -3.3302E-12  5.1659E-11 -3.4064E-09
 -1.3864E-11 -3.0281E-08 -3.3302E-12  2.4404E-10 -4.6018E-09  3.0341E-07
  2.9033E-10  6.1596E-07  5.1659E-11 -4.6018E-09  9.3718E-08 -6.1470E-06
 -1.8602E-08 -4.0441E-05 -3.4064E-09  3.0341E-07 -6.1470E-06  4.0496E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
    0.125614 -179.484422    0.054815    0.002300   -0.990635  2457099.974968
# Heliocentric elements and errors
Epoch:              2457090.5000  =  2015/03/09
Mean Anomaly:          306.64467 +/-   132.744
Argument of Peri:       61.20865 +/-   192.006
Long of Asc Node:      179.66685 +/-     0.052
Inclination:             9.13603 +/-     0.607
Eccentricity:         0.07348101 +/-    0.6310
Semi-Major Axis:     36.91043455 +/-    6.5283
Time of Perihelion: 2469229.9060 +/-   30029.7
Perihelion:          34.19821847 +/-   24.0636
Aphelion:            39.62265064 +/-   24.3225
Period (y)              224.2497 +/-     59.49
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -35.42577005 +/-    0.3629
Ecliptic Y           -0.26407948 +/-    0.0032
Ecliptic Z            0.07559490 +/-    0.0008
Ecliptic XDOT         0.00020411 +/-    0.0019
Ecliptic YDOT        -0.00290328 +/-    0.0001
Ecliptic ZDOT         0.00046670 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   35.42683497 +/-    0.3629
Geocenter to KBO     34.43303699 +/-    0.3630
# Hcoef:  7.71

The following table shows the complete astrometric record for 15FF490. 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 (15FF490) followed by the observatory code and reference code for the source of the astrometry.

2015 03  18.47419  12 02 05.52   -00 05 23.4   23.3r 15FF490   T09  C~8eRh      
2015 03  18.50126  12 02 05.37   -00 05 22.5   23.2r 15FF490   T09  C~8eRh      
2015 03  18.50997  12 02 05.33   -00 05 22.2   23.2r 15FF490   T09  C~8eRh      
2015 03  18.53616  12 02 05.19   -00 05 21.0   23.2r 15FF490   T09  C~8eRh      
2015 03  18.56659  12 02 05.02   -00 05 20.2   23.1r 15FF490   T09  C~8eRh      
2015 03  20.41961  12 01 55.44   -00 04 11.8   22.8i 15FF490   T09  C~8eRh      
2015 03  20.49142  12 01 55.06   -00 04 09.1   22.9i 15FF490   T09  C~8eRh      
2015 03  25.48707  12 01 29.14   -00 01 05.4   24.3g 15FF490   T09  C~8eRh      
2015 03  25.51323  12 01 29.00   -00 01 04.5   23.9g 15FF490   T09  C~8eRh      
2015 03  25.54330  12 01 28.85   -00 01 03.4   24.0g 15FF490   T09  C~8eRh      
2015 03  25.55400  12 01 28.79   -00 01 03.0   24.2g 15FF490   T09  C~8eRh      
2015 03  29.25932  12 01 09.70   +00 01 12.3   22.6y 15FF490   T09  C~8eRh      
2015 03  29.27997  12 01 09.62   +00 01 13.1   22.1y 15FF490   T09  C~8eRh      
2015 03  29.29907  12 01 09.50   +00 01 13.6   22.5y 15FF490   T09  C~8eRh      
2015 03  29.31534  12 01 09.42   +00 01 14.3   22.4y 15FF490   T09  C~8eRh      
2015 03  29.35626  12 01 09.21   +00 01 16.0   22.5y 15FF490   T09  C~8eRh      
2015 05  23.26835  11 57 39.07   +00 26 39.6   22.7z 15FF490   T09  C~8eRh      
2015 05  23.27714  11 57 39.05   +00 26 39.8   22.8z 15FF490   T09  C~8eRh      
2015 05  23.33848  11 57 38.93   +00 26 40.8   23.0z 15FF490   T09  C~8eRh      
2015 05  23.35585  11 57 38.91   +00 26 40.9   23.1z 15FF490   T09  C~8eRh      

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     -2.42    -0.03      -0.07    -0.10
     3   0.0001     -3.09     0.06      -0.03    -0.09
     4   0.0002     -5.50    -0.06       0.23     0.12
     5   0.0003     -8.15    -0.07      -0.05    -0.23
     6   0.0053   -167.20     0.06       5.55     0.09
     7   0.0055   -173.51     0.04       5.76     0.14
     8   0.0192   -603.30    -0.04      19.65     0.10
     9   0.0193   -605.58    -0.05      19.64     0.04
    10   0.0194   -608.08     0.06      19.76     0.08
    11   0.0194   -609.07     0.00      19.77     0.07
    12   0.0295   -925.61    -0.16      30.00    -0.13
    13   0.0296   -927.03     0.19      30.26     0.08
    14   0.0296   -928.88    -0.01      30.00    -0.22
    15   0.0297   -930.26     0.01      30.17    -0.09
    16   0.0298   -933.83    -0.03      30.47     0.12
    17   0.1801  -4432.52     0.05     174.68    -0.06
    18   0.1802  -4432.87    -0.02     174.75    -0.01
    19   0.1803  -4434.92    -0.13     174.95     0.07
    20   0.1804  -4435.24     0.10     174.92     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.

15FF490    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