Orbit Fit and Astrometric record for 15FE562

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: 15FE562   
# Created Mon Jul  7 01:10:33 2025
# Orbit generated from Bernstein formalism
# Fitting     23 observations of     23
# Arc:  62.83d
# First observation: 2015/01/16
#  Last observation: 2015/03/20
Preliminary a, adot, b, bdot, g, gdot:
   0.000001   0.019610   0.000000   0.002739   0.021719   0.000000
# Chi-squared of fit:    31.55 DOF:     40 RMS:  0.21
# Min/Max residuals:    -0.30    1.16
# Exact a, adot, b, bdot, g, gdot:
  1.515437E-05  1.895301E-02  2.101605E-06  2.728225E-03  2.158255E-02  3.067818E-03
# Covariance matrix:
  2.9943E-13  1.7019E-10  9.5725E-14  2.7290E-12  3.5337E-11  2.2408E-09
  1.7019E-10  3.1335E-07  1.5913E-10  4.1654E-09  5.7838E-08  1.9222E-06
  9.5725E-14  1.5913E-10  1.7381E-13  1.5581E-12  2.9674E-11  1.0703E-09
  2.7290E-12  4.1654E-09  1.5581E-12  6.9575E-11  7.8419E-10  3.0351E-08
  3.5337E-11  5.7838E-08  2.9674E-11  7.8419E-10  1.0803E-08  3.9470E-07
  2.2408E-09  1.9222E-06  1.0703E-09  3.0351E-08  3.9470E-07  2.4271E-05
#      lat0       lon0       xBary       yBary       zBary        JD0
   -8.408660  151.783681    0.577720   -0.115925   -0.785327  2457039.052368
# Heliocentric elements and errors
Epoch:              2457030.5000  =  2015/01/08
Mean Anomaly:           93.56198 +/-    58.526
Argument of Peri:      203.62051 +/-    44.920
Long of Asc Node:      196.60039 +/-     0.936
Inclination:            11.50841 +/-     0.181
Eccentricity:         0.14969893 +/-    0.2177
Semi-Major Axis:     45.70543569 +/-    4.6477
Time of Perihelion: 2427698.1324 +/-   17794.4
Perihelion:          38.86338066 +/-   10.7082
Aphelion:            52.54749071 +/-   11.2960
Period (y)              309.0011 +/-     47.13
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -40.81855044 +/-    0.1945
Ecliptic Y           22.55573459 +/-    0.1044
Ecliptic Z           -6.77542514 +/-    0.0326
Ecliptic XDOT        -0.00152446 +/-    0.0006
Ecliptic YDOT        -0.00191797 +/-    0.0003
Ecliptic ZDOT         0.00028556 +/-    0.0001
# Distances at JD0 (AU)
Heliocenter to KBO   47.12559399 +/-    0.1758
Geocenter to KBO     46.33372838 +/-    0.2231
# Hcoef:  8.72

The following table shows the complete astrometric record for 15FE562. 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 (15FE562) followed by the observatory code and reference code for the source of the astrometry.

2015 01  16.55159  10 03 10.59   +02 58 26.3   24.6z 15FE562   T09  C~8vFY      
2015 01  16.58807  10 03 10.49   +02 58 26.8   25.1z 15FE562   T09  C~8vFY      
2015 01  16.64052  10 03 10.30   +02 58 27.4   25.0z 15FE562   T09  C~8vFY      
2015 01  16.65500  10 03 10.25   +02 58 27.6   25.2z 15FE562   T09  C~8vFY      
2015 01  17.40063  10 03 07.72   +02 58 37.9   25.1i 15FE562   T09  C~8vFY      
2015 01  17.40524  10 03 07.72   +02 58 37.7   25.0i 15FE562   T09  C~8vFY      
2015 01  17.41437  10 03 07.67   +02 58 38.0   25.1i 15FE562   T09  C~8vFY      
2015 01  17.41902  10 03 07.67   +02 58 38.0   25.1i 15FE562   T09  C~8vFY      
2015 01  19.41506  10 03 00.82   +02 59 06.3   25.3z 15FE562   T09  C~8vFY      
2015 01  19.41965  10 03 00.72   +02 59 06.6   25.3z 15FE562   T09  C~8vFY      
2015 01  19.42426  10 03 00.70   +02 59 06.6   24.6z 15FE562   T09  C~8vFY      
2015 01  20.41862  10 02 57.19   +02 59 21.6   26.9g 15FE562   T09  C~8vFY      
2015 01  20.42825  10 02 57.15   +02 59 21.6   26.7g 15FE562   T09  C~8vFY      
2015 01  20.43306  10 02 57.13   +02 59 22.0   26.6g 15FE562   T09  C~8vFY      
2015 01  20.43784  10 02 57.11   +02 59 22.0   26.8g 15FE562   T09  C~8vFY      
2015 01  21.62499  10 02 52.87   +02 59 40.0   25.0i 15FE562   T09  C~8vFY      
2015 01  21.65094  10 02 52.76   +02 59 40.3   25.3i 15FE562   T09  C~8vFY      
2015 03  18.39076  09 59 11.96   +03 21 13.3   25.3r 15FE562   T09  C~8vFY      
2015 03  18.42974  09 59 11.82   +03 21 14.3   25.5r 15FE562   T09  C~8vFY      
2015 03  18.44789  09 59 11.75   +03 21 14.9   25.5r 15FE562   T09  C~8vFY      
2015 03  20.35412  09 59 05.11   +03 22 05.0   25.1i 15FE562   T09  C~8vFY      
2015 03  20.36873  09 59 05.07   +03 22 05.3   24.6i 15FE562   T09  C~8vFY      
2015 03  20.38334  09 59 05.01   +03 22 05.8   24.9i 15FE562   T09  C~8vFY      

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    -0.26       0.00    -0.02
     2   0.0001     -1.58     0.10      -0.06     0.12
     3   0.0002     -4.45     0.01      -0.49    -0.02
     4   0.0003     -5.23     0.00      -0.57    -0.02
     5   0.0023    -44.33    -0.16      -4.23     0.03
     6   0.0023    -44.26     0.15      -4.41    -0.13
     7   0.0024    -45.06    -0.16      -4.40    -0.06
     8   0.0024    -45.06     0.09      -4.40    -0.04
     9   0.0078   -151.08     1.16     -13.91     0.18
    10   0.0079   -152.59    -0.10     -14.15    -0.05
    11   0.0079   -152.87    -0.12     -14.26    -0.13
    12   0.0106   -207.37    -0.11     -18.66     0.06
    13   0.0106   -207.93    -0.14     -18.87    -0.10
    14   0.0106   -208.35    -0.29     -18.61     0.19
    15   0.0106   -208.63    -0.30     -18.71     0.11
    16   0.0139   -274.42     0.15     -24.14     0.02
    17   0.0140   -276.07    -0.02     -24.44    -0.16
    18   0.1666  -3826.84     0.01      27.43     0.00
    19   0.1667  -3829.15     0.03      27.63    -0.02
    20   0.1667  -3830.34    -0.08      27.83     0.07
    21   0.1719  -3941.06    -0.06      39.95    -0.03
    22   0.1720  -3941.73     0.13      40.02    -0.04
    23   0.1720  -3942.74    -0.03      40.18     0.02

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.

15FE562    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