Orbit Fit and Astrometric record for 15FB490

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: 15FB490   
# Created Sun Feb 23 02:10:20 2025
# Orbit generated from Bernstein formalism
# Fitting     22 observations of     22
# Arc:  65.89d
# First observation: 2015/03/18
#  Last observation: 2015/05/23
Preliminary a, adot, b, bdot, g, gdot:
  -0.000000   0.028678   0.000000   0.000108   0.024354   0.000000
# WARNING Fitting with energy constraint
# Chi-squared of fit:     8.71 DOF:     39 RMS:  0.11
# Min/Max residuals:    -0.27    0.18
# Exact a, adot, b, bdot, g, gdot:
  1.460768E-05  2.160470E-02  3.868212E-07  1.153215E-04  2.323425E-02  4.420742E-03
# Covariance matrix:
  1.6674E-12  2.5871E-09  4.2888E-14 -2.8157E-12  3.9411E-10 -3.1313E-08
  2.5871E-09  4.7627E-06  7.9216E-11 -5.2037E-09  7.2200E-07 -5.8527E-05
  4.2888E-14  7.9216E-11  1.0294E-13 -8.4623E-13  1.2007E-11 -9.7393E-10
 -2.8157E-12 -5.2037E-09 -8.4623E-13  2.2396E-11 -7.8872E-10  6.3983E-08
  3.9411E-10  7.2200E-07  1.2007E-11 -7.8872E-10  1.0947E-07 -8.8669E-06
 -3.1313E-08 -5.8527E-05 -9.7393E-10  6.3983E-08 -8.8669E-06  7.2071E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.081463 -179.741108    0.050325   -0.001281   -0.990876  2457099.977938
# Heliocentric elements and errors
Epoch:              2457090.5000  =  2015/03/09
Mean Anomaly:           75.70577 +/-   115.492
Argument of Peri:      246.64297 +/-    11.051
Long of Asc Node:      194.73991 +/-     1.634
Inclination:             0.31685 +/-     0.035
Eccentricity:         0.20041106 +/-    1.1994
Semi-Major Axis:     44.46829591 +/-   15.9456
Time of Perihelion: 2434313.2856 +/-   32516.0
Perihelion:          35.55635743 +/-   54.8391
Aphelion:            53.38023439 +/-   56.6671
Period (y)              296.5404 +/-    159.50
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -44.03363903 +/-    0.6129
Ecliptic Y           -0.14882279 +/-    0.0027
Ecliptic Z           -0.06116125 +/-    0.0009
Ecliptic XDOT        -0.00051285 +/-    0.0032
Ecliptic YDOT        -0.00255393 +/-    0.0002
Ecliptic ZDOT         0.00001294 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   44.03393299 +/-    0.6129
Geocenter to KBO     43.03990643 +/-    0.6129
# Hcoef:  7.61

The following table shows the complete astrometric record for 15FB490. 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 (15FB490) followed by the observatory code and reference code for the source of the astrometry.

2015 03  18.47716  12 00 49.23   -00 10 39.8   24.1r 15FB490   T09  C~8eRg      
2015 03  18.50997  12 00 49.08   -00 10 38.8   23.8r 15FB490   T09  C~8eRh      
2015 03  18.56659  12 00 48.84   -00 10 37.3   23.8r 15FB490   T09  C~8eRh      
2015 03  20.42312  12 00 40.85   -00 09 44.9   23.4i 15FB490   T09  C~8eRh      
2015 03  20.46343  12 00 40.67   -00 09 43.9   23.3i 15FB490   T09  C~8eRh      
2015 03  20.49142  12 00 40.54   -00 09 43.4   23.5i 15FB490   T09  C~8eRh      
2015 03  20.50240  12 00 40.49   -00 09 42.9   23.4i 15FB490   T09  C~8eRh      
2015 03  25.48707  12 00 19.02   -00 07 22.8   25.3g 15FB490   T09  C~8eRh      
2015 03  25.51323  12 00 18.88   -00 07 22.0   25.1g 15FB490   T09  C~8eRh      
2015 03  25.51534  12 00 18.89   -00 07 22.0   24.7g 15FB490   T09  C~8eRh      
2015 03  25.54330  12 00 18.78   -00 07 21.1   25.5g 15FB490   T09  C~8eRh      
2015 03  29.27997  12 00 02.78   -00 05 37.0   23.9y 15FB490   T09  C~8eRh      
2015 03  29.29907  12 00 02.71   -00 05 36.3   24.0y 15FB490   T09  C~8eRh      
2015 03  29.31803  12 00 02.63   -00 05 36.0   23.1y 15FB490   T09  C~8eRh      
2015 03  29.33718  12 00 02.54   -00 05 35.1   23.6y 15FB490   T09  C~8eRh      
2015 03  29.33991  12 00 02.54   -00 05 35.1   23.1y 15FB490   T09  C~8eRh      
2015 03  29.35626  12 00 02.45   -00 05 34.6   24.1y 15FB490   T09  C~8eRh      
2015 03  29.42373  12 00 02.16   -00 05 32.8   23.4y 15FB490   T09  C~8eRh      
2015 05  23.27714  11 57 06.11   +00 13 39.3   23.4z 15FB490   T09  C~8eRh      
2015 05  23.29468  11 57 06.09   +00 13 39.8   23.9z 15FB490   T09  C~8eRh      
2015 05  23.33848  11 57 06.01   +00 13 40.1   23.6z 15FB490   T09  C~8eRh      
2015 05  23.36453  11 57 05.97   +00 13 40.4   23.8z 15FB490   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     0.02       0.00    -0.06
     2   0.0001     -2.46    -0.10       0.02    -0.03
     3   0.0002     -6.36     0.05      -0.03    -0.06
     4   0.0053   -137.16     0.01       0.37     0.18
     5   0.0054   -140.04     0.03       0.21     0.04
     6   0.0055   -142.03     0.04      -0.10    -0.27
     7   0.0055   -142.91    -0.06       0.06    -0.10
     8   0.0192   -494.12     0.12       0.49     0.03
     9   0.0193   -496.36    -0.26       0.39    -0.07
    10   0.0193   -496.23     0.02       0.45    -0.00
    11   0.0193   -498.10     0.14       0.62     0.17
    12   0.0296   -759.70    -0.05       0.66    -0.17
    13   0.0296   -760.95     0.06       0.89     0.06
    14   0.0297   -762.17     0.17       0.68    -0.13
    15   0.0297   -763.76    -0.07       0.97     0.16
    16   0.0297   -763.76     0.12       0.97     0.16
    17   0.0298   -765.20    -0.16       0.89     0.09
    18   0.0300   -769.91    -0.09       0.82     0.04
    19   0.1802  -3651.40     0.01       7.41    -0.19
    20   0.1802  -3651.87     0.01       7.75     0.16
    21   0.1803  -3653.10    -0.03       7.55    -0.03
    22   0.1804  -3653.77    -0.00       7.58     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.

15FB490    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