Orbit Fit and Astrometric record for 15FN496

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: 15FN496   
# Created Sun Apr 27 01:10:23 2025
# Orbit generated from Bernstein formalism
# Fitting     23 observations of     23
# Arc:   1.15y
# First observation: 2015/01/16
#  Last observation: 2016/03/12
Preliminary a, adot, b, bdot, g, gdot:
  -0.000013   0.024694  -0.000008  -0.015249   0.026451   0.000000
# Chi-squared of fit:    12.16 DOF:     40 RMS:  0.13
# Min/Max residuals:    -0.36    0.26
# Exact a, adot, b, bdot, g, gdot:
  1.380644E-05  2.483454E-02 -1.019059E-05 -1.539240E-02  2.659782E-02  7.602172E-03
# Covariance matrix:
  1.7766E-13  1.4171E-13  1.7723E-14 -3.0758E-13  2.7712E-13  1.7009E-11
  1.4171E-13  4.0690E-12  4.5793E-13 -7.2718E-12  2.6089E-12  4.0329E-10
  1.7723E-14  4.5793E-13  1.5834E-13 -1.0149E-12  2.9512E-13  5.0614E-11
 -3.0758E-13 -7.2718E-12 -1.0149E-12  1.4710E-11 -4.7327E-12 -7.9988E-10
  2.7712E-13  2.6089E-12  2.9512E-13 -4.7327E-12  1.9932E-12  2.6238E-10
  1.7009E-11  4.0329E-10  5.0614E-11 -7.9988E-10  2.6238E-10  4.4368E-08
#      lat0       lon0       xBary       yBary       zBary        JD0
  -16.154313  139.715497    0.400487   -0.249243   -0.861067  2457038.959318
# Heliocentric elements and errors
Epoch:              2457030.5000  =  2015/01/08
Mean Anomaly:           28.41315 +/-     0.303
Argument of Peri:      150.77552 +/-     0.715
Long of Asc Node:      295.49303 +/-     0.004
Inclination:            35.21392 +/-     0.004
Eccentricity:         0.34761476 +/-    0.0074
Semi-Major Axis:     51.95152638 +/-    0.3152
Time of Perihelion: 2446235.7441 +/-      59.9
Perihelion:          33.89240901 +/-    0.4346
Aphelion:            70.01064376 +/-    0.5719
Period (y)              374.4602 +/-      3.41
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -27.97626301 +/-    0.0015
Ecliptic Y           24.23521741 +/-    0.0012
Ecliptic Z          -10.46085084 +/-    0.0006
Ecliptic XDOT        -0.00189387 +/-    0.0000
Ecliptic YDOT        -0.00175447 +/-    0.0000
Ecliptic ZDOT        -0.00173948 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   38.46357309 +/-    0.0013
Geocenter to KBO     37.59706130 +/-    0.0020
# Hcoef:  8.58

The following table shows the complete astrometric record for 15FN496. 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 (15FN496) followed by the observatory code and reference code for the source of the astrometry.

2015 01  16.45854  09 08 28.14   -00 28 16.7   24.2z 15FN496   T09  C~8nc2      
2015 01  16.49318  09 08 27.94   -00 28 16.7   23.7z 15FN496   T09  C~8nc2      
2015 01  16.50404  09 08 27.88   -00 28 16.7   24.0z 15FN496   T09  C~8nc2      
2015 01  16.51495  09 08 27.84   -00 28 16.7   24.3z 15FN496   T09  C~8nc2      
2015 01  21.43754  09 08 02.49   -00 27 51.2   24.0i 15FN496   T09  C~8nc2      
2015 01  21.48977  09 08 02.21   -00 27 51.0   23.8i 15FN496   T09  C~8nc2      
2015 01  21.52648  09 08 02.01   -00 27 50.7   24.3i 15FN496   T09  C~8nc2      
2015 01  27.39521  09 07 30.98   -00 27 01.7   23.8y 15FN496   T09  C~8nc2      
2015 01  27.45286  09 07 30.66   -00 27 01.2   23.7y 15FN496   T09  C~8nc2      
2015 01  27.52703  09 07 30.25   -00 27 00.7   23.7y 15FN496   T09  C~8nc2      
2015 03  18.32647  09 03 26.31   -00 10 33.8   24.6r 15FN496   T09  C~8nc2      
2015 03  18.34385  09 03 26.25   -00 10 33.1   24.8r 15FN496   T09  C~8nc2      
2015 03  18.35901  09 03 26.19   -00 10 33.0   24.8r 15FN496   T09  C~8nc2      
2015 03  18.36116  09 03 26.18   -00 10 33.0   25.0r 15FN496   T09  C~8nc2      
2015 03  25.39368  09 03 02.07   -00 07 36.4   25.2g 15FN496   T09  C~8nc2      
2015 03  25.40864  09 03 02.03   -00 07 35.7   25.6g 15FN496   T09  C~8nc2      
2015 03  25.41932  09 03 01.99   -00 07 35.7   25.0g 15FN496   T09  C~8nc2      
2016 03  04.30541  09 08 43.05   -01 31 54.3   24.4i 15FN496   T09  C~8nc2      
2016 03  04.32261  09 08 42.98   -01 31 54.0   24.1i 15FN496   T09  C~8nc2      
2016 03  12.23749  09 08 08.44   -01 28 34.3   24.2z 15FN496   T09  C~8nc2      
2016 03  12.24703  09 08 08.38   -01 28 34.1   24.3z 15FN496   T09  C~8nc2      
2016 03  12.27134  09 08 08.30   -01 28 33.5   23.9z 15FN496   T09  C~8nc2      
2016 03  12.28216  09 08 08.28   -01 28 33.0   24.6z 15FN496   T09  C~8nc2      

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     0.20       0.00     0.21
     2   0.0001     -2.86    -0.07      -0.91    -0.00
     3   0.0001     -3.72    -0.11      -1.18    -0.06
     4   0.0002     -4.29     0.13      -1.37    -0.02
     5   0.0136   -374.33    -0.05     -92.45     0.15
     6   0.0138   -378.40    -0.04     -93.54     0.00
     7   0.0139   -381.35    -0.12     -94.16     0.04
     8   0.0299   -839.70     0.07    -188.72     0.09
     9   0.0301   -844.43    -0.00    -189.70    -0.01
    10   0.0303   -850.44    -0.03    -191.09    -0.28
    11   0.1666  -4637.19    -0.06    -361.45    -0.08
    12   0.1667  -4638.26    -0.06    -361.06     0.20
    13   0.1667  -4639.15    -0.01    -361.24    -0.08
    14   0.1667  -4639.29    -0.02    -361.28    -0.14
    15   0.1860  -5037.70     0.04    -302.79    -0.16
    16   0.1860  -5038.49     0.06    -302.31     0.19
    17   0.1861  -5039.06     0.06    -302.49    -0.09
    18   1.1303   1371.66     0.02   -3570.15     0.04
    19   1.1304   1370.56     0.21   -3570.18    -0.03
    20   1.1520    816.37    -0.09   -3537.03    -0.01
    21   1.1521    815.45    -0.36   -3537.11    -0.15
    22   1.1521    814.12    -0.04   -3536.91    -0.07
    23   1.1522    813.68     0.26   -3536.52     0.25

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.

15FN496    quality flag:3

Type:       SCATNEAR  SCATNEAR  SCATNEAR

axisobj        51.802    52.802    50.892
ecceobj         0.348     0.369     0.327
incobj         35.254    35.266    35.241
qmin           31.780    31.604    32.558
qmax           72.792    74.613    69.537
amean          51.846    52.501    50.659
amin           51.059    51.683    50.149
amax           52.542    53.332    51.303
emean           0.360     0.369     0.333
emin            0.327     0.346     0.310
emax            0.386     0.399     0.356
imean          36.405    36.686    36.515
imin           35.673    35.883    35.888
imax           37.378    37.400    37.239
excite_mean     0.694     0.702     0.682
fracstop        1.000     1.000     1.000
cjmean          2.550     2.541     2.559

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       197.1     178.1     182.6
kozaiamp        180.0     180.0     180.0