Orbit Fit and Astrometric record for 15FB562

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: 15FB562   
# Created Mon Jul  7 01:10:33 2025
# Orbit generated from Bernstein formalism
# Fitting     23 observations of     23
# Arc:  63.90d
# First observation: 2015/03/18
#  Last observation: 2015/05/21
Preliminary a, adot, b, bdot, g, gdot:
  -0.000003   0.023142   0.000001  -0.005422   0.023043   0.000000
# WARNING Fitting with energy constraint
# Chi-squared of fit:    14.59 DOF:     41 RMS:  0.14
# Min/Max residuals:    -0.23    0.53
# Exact a, adot, b, bdot, g, gdot:
  1.495772E-05  2.185253E-02 -3.414951E-06 -5.127319E-03  2.299818E-02  5.742525E-03
# Covariance matrix:
  3.3406E-13 -7.2878E-12 -1.0039E-14  1.2301E-12  4.6254E-12  2.1881E-09
 -7.2878E-12  1.1693E-08  5.3824E-12 -2.6735E-09  9.4173E-10 -8.7113E-07
 -1.0039E-14  5.3824E-12  2.5333E-13 -2.6966E-12 -2.9065E-14 -5.6087E-10
  1.2301E-12 -2.6735E-09 -2.6966E-12  6.2379E-10 -2.2186E-10  1.9720E-07
  4.6254E-12  9.4173E-10 -2.9065E-14 -2.2186E-10  3.9638E-10  4.0137E-08
  2.1881E-09 -8.7113E-07 -5.6087E-10  1.9720E-07  4.0137E-08  1.0298E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
   -9.350287  152.501493   -0.415720   -0.146225   -0.888888  2457099.901368
# Heliocentric elements and errors
Epoch:              2457090.5000  =  2015/03/09
Mean Anomaly:           45.46253 +/-    19.782
Argument of Peri:      139.43666 +/-    26.624
Long of Asc Node:      298.79883 +/-     0.297
Inclination:            15.98876 +/-     0.115
Eccentricity:         0.29199108 +/-    0.4631
Semi-Major Axis:     51.96954054 +/-   14.5277
Time of Perihelion: 2439809.3438 +/-    2009.3
Perihelion:          36.79489828 +/-   26.1719
Aphelion:            67.14418281 +/-   30.5200
Period (y)              374.6550 +/-    157.10
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -39.05122513 +/-    0.0329
Ecliptic Y           19.85689449 +/-    0.0172
Ecliptic Z           -7.06460543 +/-    0.0061
Ecliptic XDOT        -0.00171495 +/-    0.0011
Ecliptic YDOT        -0.00204766 +/-    0.0006
Ecliptic ZDOT        -0.00071326 +/-    0.0002
# Distances at JD0 (AU)
Heliocenter to KBO   44.37570386 +/-    0.0300
Geocenter to KBO     43.48170080 +/-    0.0376
# Hcoef:  8.73

The following table shows the complete astrometric record for 15FB562. 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 (15FB562) followed by the observatory code and reference code for the source of the astrometry.

2015 03  18.40059  10 04 30.43   +01 50 34.7   25.2r 15FB562   T09  C~8vFX      
2015 03  18.41927  10 04 30.34   +01 50 35.2   25.3r 15FB562   T09  C~8vFX      
2015 03  18.43740  10 04 30.29   +01 50 35.6   24.9r 15FB562   T09  C~8vFX      
2015 03  20.35051  10 04 23.01   +01 51 22.4   24.6i 15FB562   T09  C~8vFX      
2015 03  20.37966  10 04 22.90   +01 51 23.2   24.2i 15FB562   T09  C~8vFX      
2015 03  20.39412  10 04 22.84   +01 51 23.2   23.7i 15FB562   T09  C~8vFX      
2015 05  17.25906  10 02 35.01   +02 09 01.2   26.6g 15FB562   T09  C~8vFX      
2015 05  17.26292  10 02 35.01   +02 09 01.0   26.2g 15FB562   T09  C~8vFX      
2015 05  17.27711  10 02 35.03   +02 09 01.0   26.1g 15FB562   T09  C~8vFX      
2015 05  17.28396  10 02 35.02   +02 09 01.5   26.2g 15FB562   T09  C~8vFX      
2015 05  17.29799  10 02 35.06   +02 09 01.8   26.5g 15FB562   T09  C~8vFX      
2015 05  17.31259  10 02 35.03   +02 09 01.5   25.8g 15FB562   T09  C~8vFX      
2015 05  21.25350  10 02 37.31   +02 09 29.9   24.8i 15FB562   T09  C~8vFX      
2015 05  21.25735  10 02 37.29   +02 09 29.9   25.3i 15FB562   T09  C~8vFX      
2015 05  21.26121  10 02 37.30   +02 09 30.2   25.3i 15FB562   T09  C~8vFX      
2015 05  21.26506  10 02 37.30   +02 09 29.9   24.7i 15FB562   T09  C~8vFX      
2015 05  21.27277  10 02 37.31   +02 09 29.9   25.1i 15FB562   T09  C~8vFX      
2015 05  21.27663  10 02 37.30   +02 09 30.2   25.0i 15FB562   T09  C~8vFX      
2015 05  21.28048  10 02 37.31   +02 09 30.1   24.8i 15FB562   T09  C~8vFX      
2015 05  21.28433  10 02 37.31   +02 09 30.2   25.4i 15FB562   T09  C~8vFX      
2015 05  21.28819  10 02 37.31   +02 09 30.2   25.1i 15FB562   T09  C~8vFX      
2015 05  21.29204  10 02 37.32   +02 09 30.2   25.0i 15FB562   T09  C~8vFX      
2015 05  21.29589  10 02 37.32   +02 09 30.2   24.6i 15FB562   T09  C~8vFX      

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     0.01       0.00    -0.02
     2   0.0001     -1.44    -0.23      -0.01    -0.07
     3   0.0001     -2.28     0.08       0.10     0.00
     4   0.0053   -120.92     0.03       5.36     0.08
     5   0.0054   -122.74     0.03       5.53     0.17
     6   0.0055   -123.59     0.09       5.21    -0.18
     7   0.1639  -2009.47    -0.16     424.75     0.07
     8   0.1639  -2009.40    -0.10     424.56    -0.15
     9   0.1639  -2009.12     0.16     424.67    -0.18
    10   0.1640  -2009.43    -0.17     425.08     0.17
    11   0.1640  -2008.98     0.26     425.57     0.53
    12   0.1640  -2009.29    -0.09     425.13    -0.05
    13   0.1748  -1987.33     0.27     463.77     0.02
    14   0.1748  -1987.61    -0.04     463.66    -0.13
    15   0.1748  -1987.58    -0.03     463.99     0.17
    16   0.1749  -1987.47     0.04     463.71    -0.15
    17   0.1749  -1987.33     0.13     463.77    -0.17
    18   0.1749  -1987.58    -0.15     463.99     0.03
    19   0.1749  -1987.40     0.00     463.95    -0.05
    20   0.1749  -1987.44    -0.06     464.05     0.01
    21   0.1749  -1987.44    -0.09     464.05    -0.03
    22   0.1749  -1987.30     0.02     464.10    -0.01
    23   0.1749  -1987.30    -0.01     464.10    -0.05

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.

15FB562    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