Orbit Fit and Astrometric record for 15FE490

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: 15FE490   
# Created Sun Feb 23 02:10:20 2025
# Orbit generated from Bernstein formalism
# Fitting     24 observations of     24
# Arc:  10.88d
# First observation: 2015/03/18
#  Last observation: 2015/03/29
Preliminary a, adot, b, bdot, g, gdot:
   0.000001   0.013449  -0.000001   0.004374   0.020299   0.000000
# WARNING Fitting with energy constraint
# WARNING MRQMIN stopped after  16 iterations -- oscilliatory solution
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# Chi-squared of fit:     7.49 DOF:     43 RMS:  0.10
# Min/Max residuals:    -0.25    0.21
# Exact a, adot, b, bdot, g, gdot:
  1.370891E-05  1.642711E-02  2.791329E-06  4.372972E-03  2.076760E-02 -8.698555E-03
# Covariance matrix:
  7.3313E-11  9.3730E-08 -7.1755E-14  1.4205E-11  1.4943E-08  8.6466E-08
  9.3730E-08  1.2010E-04 -9.1407E-11  1.8026E-08  1.9145E-05  1.0948E-04
 -7.1755E-14 -9.1407E-11  1.3973E-13 -6.2162E-12 -1.4589E-11 -1.1688E-10
  1.4205E-11  1.8026E-08 -6.2162E-12  4.9385E-10  2.8794E-09  2.7486E-08
  1.4943E-08  1.9145E-05 -1.4589E-11  2.8794E-09  3.0518E-06  1.7497E-05
  8.6466E-08  1.0948E-04 -1.1688E-10  2.7486E-08  1.7497E-05  1.8276E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
    0.248702 -178.716121    0.068094    0.004425   -0.989804  2457099.974968
# Heliocentric elements and errors
Epoch:              2457090.5000  =  2015/03/09
Mean Anomaly:          302.93024 +/-    55.751
Argument of Peri:      111.81910 +/-    84.514
Long of Asc Node:      180.28696 +/-     0.616
Inclination:            14.88142 +/-     9.473
Eccentricity:         0.45739143 +/-    0.7367
Semi-Major Axis:     52.02011101 +/-   27.4589
Time of Perihelion: 2478815.4541 +/-   12430.6
Perihelion:          28.22655800 +/-   41.1177
Aphelion:            75.81366403 +/-   55.4089
Period (y)              375.2020 +/-    297.08
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -49.13359426 +/-    4.0494
Ecliptic Y           -1.03321020 +/-    0.0904
Ecliptic Z            0.20916146 +/-    0.0176
Ecliptic XDOT         0.00119406 +/-    0.0018
Ecliptic YDOT        -0.00214511 +/-    0.0013
Ecliptic ZDOT         0.00057161 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   49.14490164 +/-    4.0485
Geocenter to KBO     48.15193632 +/-    4.0505
# Hcoef:  7.26

The following table shows the complete astrometric record for 15FE490. 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 (15FE490) followed by the observatory code and reference code for the source of the astrometry.

2015 03  18.47419  12 05 06.45   -00 16 56.9   24.5r 15FE490   T09  C~8eRh      
2015 03  18.50126  12 05 06.35   -00 16 56.4   24.1r 15FE490   T09  C~8eRh      
2015 03  18.53399  12 05 06.23   -00 16 55.4   24.3r 15FE490   T09  C~8eRh      
2015 03  18.53616  12 05 06.22   -00 16 55.4   24.1r 15FE490   T09  C~8eRh      
2015 03  18.56444  12 05 06.12   -00 16 54.6   24.1r 15FE490   T09  C~8eRh      
2015 03  20.41961  12 04 58.91   -00 16 02.7   23.7i 15FE490   T09  C~8eRh      
2015 03  20.46072  12 04 58.75   -00 16 01.7   23.7i 15FE490   T09  C~8eRh      
2015 03  20.49422  12 04 58.61   -00 16 00.7   23.6i 15FE490   T09  C~8eRh      
2015 03  20.49965  12 04 58.59   -00 16 00.3   23.6i 15FE490   T09  C~8eRh      
2015 03  20.53554  12 04 58.44   -00 15 59.5   23.5i 15FE490   T09  C~8eRh      
2015 03  20.53830  12 04 58.44   -00 15 59.5   23.6i 15FE490   T09  C~8eRh      
2015 03  22.47399  12 04 50.91   -00 15 05.1   23.9i 15FE490   T09  C~8eRh      
2015 03  22.49345  12 04 50.84   -00 15 04.6   23.7i 15FE490   T09  C~8eRh      
2015 03  22.51021  12 04 50.78   -00 15 04.2   23.8i 15FE490   T09  C~8eRh      
2015 03  25.48492  12 04 39.19   -00 13 40.9   25.2g 15FE490   T09  C~8eRh      
2015 03  25.51107  12 04 39.11   -00 13 40.3   25.2g 15FE490   T09  C~8eRh      
2015 03  25.51323  12 04 39.08   -00 13 40.3   25.2g 15FE490   T09  C~8eRh      
2015 03  25.55400  12 04 38.93   -00 13 38.9   25.0g 15FE490   T09  C~8eRh      
2015 03  29.25584  12 04 24.61   -00 11 56.1   23.7y 15FE490   T09  C~8eRh      
2015 03  29.27727  12 04 24.52   -00 11 55.4   23.2y 15FE490   T09  C~8eRh      
2015 03  29.31534  12 04 24.38   -00 11 54.3   23.1y 15FE490   T09  C~8eRh      
2015 03  29.33446  12 04 24.30   -00 11 53.8   23.8y 15FE490   T09  C~8eRh      
2015 03  29.35353  12 04 24.23   -00 11 53.1   23.2y 15FE490   T09  C~8eRh      
2015 03  29.35897  12 04 24.20   -00 11 53.1   23.9y 15FE490   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    -0.25       0.00     0.11
     2   0.0001     -1.58    -0.05      -0.14    -0.08
     3   0.0002     -3.62     0.04       0.06     0.05
     4   0.0002     -3.76     0.04       0.00    -0.01
     5   0.0002     -5.46     0.20       0.14     0.06
     6   0.0053   -125.33     0.01       4.75     0.00
     7   0.0054   -127.92     0.11       4.72    -0.12
     8   0.0055   -130.25    -0.01       4.80    -0.10
     9   0.0055   -130.68    -0.09       5.05     0.13
    10   0.0056   -133.07    -0.12       4.88    -0.10
    11   0.0057   -133.07     0.06       4.88    -0.11
    12   0.0110   -258.33    -0.06       9.88     0.07
    13   0.0110   -259.50     0.05       9.92     0.07
    14   0.0111   -260.48     0.17       9.93     0.05
    15   0.0192   -453.12    -0.16      17.22     0.01
    16   0.0193   -454.46     0.21      17.30     0.03
    17   0.0193   -454.87    -0.06      17.12    -0.16
    18   0.0194   -457.49    -0.02      17.51     0.15
    19   0.0295   -695.46     0.08      26.40    -0.12
    20   0.0296   -696.98    -0.05      26.51    -0.06
    21   0.0297   -699.34     0.05      26.68     0.04
    22   0.0297   -700.64    -0.01      26.66    -0.02
    23   0.0298   -701.88    -0.01      26.89     0.16
    24   0.0298   -702.29    -0.07      26.71    -0.03

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.

15FE490    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