Orbit Fit and Astrometric record for 15FS486

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: 15FS486   
# Created Sun Feb 23 02:10:20 2025
# Orbit generated from Bernstein formalism
# Fitting     23 observations of     23
# Arc:  65.89d
# First observation: 2015/03/18
#  Last observation: 2015/05/23
Preliminary a, adot, b, bdot, g, gdot:
  -0.000001   0.028362   0.000000   0.001749   0.024202   0.000000
# WARNING Fitting with energy constraint
# Chi-squared of fit:     9.19 DOF:     41 RMS:  0.11
# Min/Max residuals:    -0.24    0.19
# Exact a, adot, b, bdot, g, gdot:
  1.385731E-05  2.132116E-02  1.094976E-06  1.799829E-03  2.308992E-02  7.043199E-03
# Covariance matrix:
  6.3640E-13  7.6739E-10  6.3932E-14 -5.8689E-12  1.1833E-10 -9.3287E-09
  7.6739E-10  1.2990E-06  1.1048E-10 -1.0154E-08  1.9777E-07 -1.6437E-05
  6.3932E-14  1.1048E-10  9.6238E-14 -1.5383E-12  1.6801E-11 -1.4037E-09
 -5.8689E-12 -1.0154E-08 -1.5383E-12  9.9478E-11 -1.5440E-09  1.2903E-07
  1.1833E-10  1.9777E-07  1.6801E-11 -1.5440E-09  3.0132E-08 -2.4969E-06
 -9.3287E-09 -1.6437E-05 -1.4037E-09  1.2903E-07 -2.4969E-06  2.0958E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.356741  179.452923    0.036382   -0.006045   -0.991468  2457099.977938
# Heliocentric elements and errors
Epoch:              2457090.5000  =  2015/03/09
Mean Anomaly:           58.86425 +/-    50.187
Argument of Peri:      260.23020 +/-     2.886
Long of Asc Node:      183.54010 +/-     0.232
Inclination:             4.82500 +/-     0.271
Eccentricity:         0.32007997 +/-    0.6489
Semi-Major Axis:     47.81305875 +/-   18.5534
Time of Perihelion: 2437345.0382 +/-   12301.0
Perihelion:          32.50905626 +/-   33.4926
Aphelion:            63.11706123 +/-   39.5282
Period (y)              330.6191 +/-    192.44
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -44.30035936 +/-    0.3256
Ecliptic Y            0.45919391 +/-    0.0031
Ecliptic Z           -0.26958946 +/-    0.0020
Ecliptic XDOT        -0.00086397 +/-    0.0017
Ecliptic YDOT        -0.00252579 +/-    0.0001
Ecliptic ZDOT         0.00020830 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   44.30355941 +/-    0.3255
Geocenter to KBO     43.30894870 +/-    0.3256
# Hcoef:  6.55

The following table shows the complete astrometric record for 15FS486. 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 (15FS486) followed by the observatory code and reference code for the source of the astrometry.

2015 03  18.47716  11 57 25.48   -00 06 34.9   22.8r 15FS486   T09  C~8cQL      
2015 03  18.49910  11 57 25.38   -00 06 34.3   22.7r 15FS486   T09  C~8cQL      
2015 03  18.53831  11 57 25.20   -00 06 32.9   22.7r 15FS486   T09  C~8cQL      
2015 03  18.56877  11 57 25.08   -00 06 32.3   22.8r 15FS486   T09  C~8cQL      
2015 03  18.57522  11 57 25.04   -00 06 31.9   22.9r 15FS486   T09  C~8cQM      
2015 03  20.42312  11 57 17.17   -00 05 38.7   22.3i 15FS486   T09  C~8cQM      
2015 03  20.42657  11 57 17.15   -00 05 38.7   22.4i 15FS486   T09  C~8cQM      
2015 03  20.46619  11 57 16.98   -00 05 37.5   22.5i 15FS486   T09  C~8cQM      
2015 03  20.48863  11 57 16.88   -00 05 37.0   22.6i 15FS486   T09  C~8cQM      
2015 03  20.54104  11 57 16.64   -00 05 35.5   22.8i 15FS486   T09  C~8cQM      
2015 03  25.45464  11 56 55.72   -00 03 13.7   23.8g 15FS486   T09  C~8cQM      
2015 03  25.45755  11 56 55.72   -00 03 13.7   23.8g 15FS486   T09  C~8cQM      
2015 03  25.48926  11 56 55.58   -00 03 12.7   24.1g 15FS486   T09  C~8cQM      
2015 03  25.51534  11 56 55.46   -00 03 12.0   24.0g 15FS486   T09  C~8cQM      
2015 03  25.54542  11 56 55.33   -00 03 11.0   23.7g 15FS486   T09  C~8cQM      
2015 03  25.55185  11 56 55.31   -00 03 10.9   23.6g 15FS486   T09  C~8cQM      
2015 03  29.31803  11 56 39.40   -00 01 22.8   22.3y 15FS486   T09  C~8cQM      
2015 03  29.38231  11 56 39.12   -00 01 21.3   22.3y 15FS486   T09  C~8cQM      
2015 03  29.40670  11 56 39.04   -00 01 20.5   22.2y 15FS486   T09  C~8cQM      
2015 03  29.42099  11 56 38.97   -00 01 20.2   22.0y 15FS486   T09  C~8cQM      
2015 05  23.33848  11 53 47.50   +00 18 31.1   22.8z 15FS486   T09  C~8cQM      
2015 05  23.35297  11 53 47.49   +00 18 31.3   23.1z 15FS486   T09  C~8cQM      
2015 05  23.36453  11 53 47.44   +00 18 31.3   23.0z 15FS486   T09  C~8cQM      

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     0.15       0.00     0.03
     2   0.0001     -1.61     0.10      -0.05    -0.03
     3   0.0002     -4.65    -0.14       0.16     0.16
     4   0.0003     -6.54     0.13      -0.00    -0.03
     5   0.0003     -7.25    -0.12       0.13     0.10
     6   0.0053   -136.72    -0.00       1.98     0.06
     7   0.0053   -136.99    -0.03       1.86    -0.07
     8   0.0054   -139.81    -0.02       1.95     0.00
     9   0.0055   -141.39     0.00       1.81    -0.15
    10   0.0057   -145.29    -0.16       1.76    -0.24
    11   0.0191   -489.60    -0.06       7.04    -0.02
    12   0.0191   -489.60     0.15       7.04    -0.02
    13   0.0192   -491.92     0.07       7.12     0.05
    14   0.0193   -493.85    -0.01       7.05    -0.04
    15   0.0194   -496.04    -0.07       7.19     0.08
    16   0.0194   -496.35     0.07       7.16     0.04
    17   0.0297   -758.31    -0.19      11.42     0.19
    18   0.0299   -762.76    -0.13      11.12    -0.15
    19   0.0299   -764.18     0.17      11.38     0.10
    20   0.0300   -765.26     0.09      11.24    -0.05
    21   0.1803  -3599.30     0.03      81.21     0.03
    22   0.1804  -3599.51     0.18      81.34     0.14
    23   0.1804  -3600.20    -0.21      81.04    -0.17

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.

15FS486    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