Orbit Fit and Astrometric record for 15FD562

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: 15FD562   
# Created Mon Jul  7 01:10:33 2025
# Orbit generated from Bernstein formalism
# Fitting     21 observations of     21
# Arc: 123.86d
# First observation: 2015/01/17
#  Last observation: 2015/05/21
Preliminary a, adot, b, bdot, g, gdot:
  -0.000029   0.032970   0.000070   0.000144   0.026630   0.000000
# Chi-squared of fit:    17.14 DOF:     36 RMS:  0.16
# Min/Max residuals:    -0.56    0.34
# Exact a, adot, b, bdot, g, gdot:
  1.430782E-05  2.508622E-02  1.557797E-06  8.411082E-04  2.532973E-02  2.896881E-03
# Covariance matrix:
  2.7027E-13 -1.9166E-12 -1.1457E-14  1.4832E-13  1.8605E-13  6.4036E-11
 -1.9166E-12  8.4835E-10  7.5755E-12 -7.9581E-11  9.1107E-11 -1.3465E-08
 -1.1457E-14  7.5755E-12  2.6332E-13 -1.5003E-12  8.1290E-13 -1.2175E-10
  1.4832E-13 -7.9581E-11 -1.5003E-12  1.2466E-11 -8.4223E-12  1.2964E-09
  1.8605E-13  9.1107E-11  8.1290E-13 -8.4223E-12  1.1135E-11 -1.2617E-09
  6.4036E-11 -1.3465E-08 -1.2175E-10  1.2964E-09 -1.2617E-09  2.4371E-07
#      lat0       lon0       xBary       yBary       zBary        JD0
   -9.918463  152.626248    0.576982   -0.136669   -0.782576  2457039.933458
# Heliocentric elements and errors
Epoch:              2457030.5000  =  2015/01/08
Mean Anomaly:           72.99731 +/-     0.443
Argument of Peri:      195.50726 +/-     1.768
Long of Asc Node:      231.50861 +/-     0.039
Inclination:             9.87769 +/-     0.001
Eccentricity:         0.10256194 +/-    0.0195
Semi-Major Axis:     41.08782090 +/-    0.1188
Time of Perihelion: 2437524.3111 +/-      82.8
Perihelion:          36.87377442 +/-    0.8096
Aphelion:            45.30186738 +/-    0.8132
Period (y)              263.3770 +/-      1.14
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -34.97800619 +/-    0.0045
Ecliptic Y           18.75891542 +/-    0.0024
Ecliptic Z           -6.80014280 +/-    0.0009
Ecliptic XDOT        -0.00153842 +/-    0.0000
Ecliptic YDOT        -0.00226424 +/-    0.0000
Ecliptic ZDOT         0.00003572 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   40.26909195 +/-    0.0041
Geocenter to KBO     39.47929972 +/-    0.0052
# Hcoef: 10.00

The following table shows the complete astrometric record for 15FD562. 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 (15FD562) followed by the observatory code and reference code for the source of the astrometry.

2015 01  17.43268  10 04 09.88   +01 16 04.7   25.6i 15FD562   T09  C~8vFY      
2015 01  17.43723  10 04 09.84   +01 16 05.1   25.9i 15FD562   T09  C~8vFY      
2015 01  17.44180  10 04 09.84   +01 16 05.1   25.2i 15FD562   T09  C~8vFY      
2015 01  21.57962  10 03 53.11   +01 17 02.8   25.8i 15FD562   T09  C~8vFY      
2015 01  21.60626  10 03 53.01   +01 17 03.2   25.8i 15FD562   T09  C~8vFY      
2015 01  21.63213  10 03 52.86   +01 17 04.2   26.4i 15FD562   T09  C~8vFY      
2015 03  18.39734  09 59 37.75   +01 40 31.7   25.9r 15FD562   T09  C~8vFY      
2015 03  18.40838  09 59 37.72   +01 40 32.3   25.9r 15FD562   T09  C~8vFY      
2015 03  18.41671  09 59 37.69   +01 40 32.4   25.4r 15FD562   T09  C~8vFY      
2015 03  18.42254  09 59 37.64   +01 40 32.4   25.8r 15FD562   T09  C~8vFY      
2015 03  18.43485  09 59 37.61   +01 40 32.8   25.9r 15FD562   T09  C~8vFY      
2015 03  18.44066  09 59 37.57   +01 40 33.1   26.0r 15FD562   T09  C~8vFY      
2015 03  18.45301  09 59 37.53   +01 40 33.4   26.2r 15FD562   T09  C~8vFY      
2015 03  20.36143  09 59 29.84   +01 41 31.2   25.9i 15FD562   T09  C~8vFY      
2015 03  20.37600  09 59 29.80   +01 41 31.5   25.4i 15FD562   T09  C~8vFY      
2015 03  20.39052  09 59 29.73   +01 41 32.2   25.3i 15FD562   T09  C~8vFY      
2015 05  21.26891  09 57 46.97   +02 04 55.2   26.0i 15FD562   T09  C~8vFY      
2015 05  21.27277  09 57 46.97   +02 04 55.5   26.5i 15FD562   T09  C~8vFY      
2015 05  21.27663  09 57 46.97   +02 04 55.5   26.2i 15FD562   T09  C~8vFY      
2015 05  21.28048  09 57 46.99   +02 04 55.3   25.9i 15FD562   T09  C~8vFY      
2015 05  21.29589  09 57 46.99   +02 04 55.5   26.9i 15FD562   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     0.28       0.00    -0.21
     2   0.0000     -0.70    -0.15       0.16    -0.01
     3   0.0000     -0.70     0.13       0.16     0.03
     4   0.0114   -255.80     0.05     -34.50    -0.08
     5   0.0114   -257.34     0.23     -34.66    -0.02
     6   0.0115   -259.80    -0.56     -34.52     0.34
     7   0.1642  -4336.38    -0.07     -68.35    -0.11
     8   0.1642  -4337.02     0.06     -67.94     0.22
     9   0.1642  -4337.47     0.18     -68.01     0.10
    10   0.1642  -4338.17    -0.12     -68.27    -0.20
    11   0.1643  -4338.74     0.17     -68.06    -0.06
    12   0.1643  -4339.40    -0.10     -67.99    -0.03
    13   0.1643  -4340.07     0.09     -67.92    -0.04
    14   0.1696  -4468.41    -0.19     -54.52    -0.03
    15   0.1696  -4469.07     0.13     -54.45    -0.06
    16   0.1696  -4470.30    -0.12     -54.16     0.13
    17   0.3390  -6408.08     0.06     715.64    -0.08
    18   0.3391  -6408.19    -0.08     715.92     0.15
    19   0.3391  -6408.19    -0.12     715.92     0.09
    20   0.3391  -6407.84     0.19     715.84    -0.05
    21   0.3391  -6407.91    -0.04     716.02    -0.09

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.

15FD562    quality flag:2

Type:      CLASSICAL  SCATNEAR CLASSICAL

axisobj        40.883    41.378    40.608
ecceobj         0.105     0.156     0.059
incobj          9.873     9.875     9.872
qmin           33.947    32.391    35.644
qmax           48.197    51.943    45.927
amean          40.900    41.672    40.621
amin           40.527    40.985    40.285
amax           41.301    42.425    40.978
emean           0.125     0.184     0.077
emin            0.096     0.147     0.049
emax            0.169     0.224     0.121
imean          12.241    13.350    12.078
imin            9.727    10.536    10.581
imax           14.448    15.925    13.820
excite_mean     0.247     0.295     0.223
fracstop        1.000     1.000     1.000
cjmean          2.995     2.971     3.006

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       181.9     182.5     180.9
kozaiamp        180.0     180.0     180.0