Orbit Fit and Astrometric record for 15OB203

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: 15OB203   
# Created Sun Oct 19 01:11:03 2025
# Orbit generated from Bernstein formalism
# Fitting     21 observations of     21
# Arc:   1.00y
# First observation: 2015/07/12
#  Last observation: 2016/07/12
Preliminary a, adot, b, bdot, g, gdot:
  -0.000021   0.033270   0.000004  -0.005835   0.025887   0.000000
# Chi-squared of fit:     3.76 DOF:     36 RMS:  0.07
# Min/Max residuals:    -0.20    0.14
# Exact a, adot, b, bdot, g, gdot:
  1.945897E-05  3.285487E-02 -3.115396E-06 -5.762729E-03  2.622749E-02 -1.188951E-02
# Covariance matrix:
  3.7621E-13  1.2866E-11 -3.5073E-14 -2.2960E-12  6.7767E-12  3.9837E-10
  1.2866E-11  1.9666E-09 -3.0040E-12 -3.4603E-10  7.4219E-10  5.9362E-08
 -3.5073E-14 -3.0040E-12  2.2071E-13  3.1194E-13 -1.4987E-12 -9.1373E-11
 -2.2960E-12 -3.4603E-10  3.1194E-13  6.1218E-11 -1.3047E-10 -1.0447E-08
  6.7767E-12  7.4219E-10 -1.4987E-12 -1.3047E-10  3.2461E-10  2.2490E-08
  3.9837E-10  5.9362E-08 -9.1373E-11 -1.0447E-08  2.2490E-08  1.7923E-06
#      lat0       lon0       xBary       yBary       zBary        JD0
   12.003402  -22.792276    0.749738    0.143165   -0.672904  2457215.929009
# Heliocentric elements and errors
Epoch:              2457210.5000  =  2015/07/07
Mean Anomaly:          356.97844 +/-     0.955
Argument of Peri:      175.80767 +/-     3.285
Long of Asc Node:      205.62908 +/-     0.047
Inclination:            15.33870 +/-     0.011
Eccentricity:         0.81572644 +/-    0.0432
Semi-Major Axis:    181.24065689 +/-   37.8966
Time of Perihelion: 2464690.6511 +/-     285.7
Perihelion:          33.39786083 +/-   10.4938
Aphelion:           329.08345296 +/-   69.2543
Period (y)             2440.0102 +/-    765.29
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           34.72283067 +/-    0.0236
Ecliptic Y          -15.40478274 +/-    0.0099
Ecliptic Z            7.92940417 +/-    0.0055
Ecliptic XDOT         0.00032246 +/-    0.0001
Ecliptic YDOT         0.00357742 +/-    0.0001
Ecliptic ZDOT        -0.00084647 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   38.80538302 +/-    0.0215
Geocenter to KBO     38.12793955 +/-    0.0262
# Hcoef:  7.71

The following table shows the complete astrometric record for 15OB203. 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 (15OB203) followed by the observatory code and reference code for the source of the astrometry.

2015 07  12.42822  22 17 56.74   +02 17 49.8   23.7z 15OB203   T09  C~90Hj      
2015 07  12.43901  22 17 56.70   +02 17 49.8   23.6z 15OB203   T09  C~90Hj      
2015 07  12.45520  22 17 56.66   +02 17 49.7   23.2z 15OB203   T09  C~90Hj      
2015 07  12.46872  22 17 56.60   +02 17 49.5   23.4z 15OB203   T09  C~90Hj      
2015 07  20.44212  22 17 31.00   +02 16 43.1   23.3i 15OB203   T09  C~90Hj      
2015 07  20.45844  22 17 30.95   +02 16 42.9   23.3i 15OB203   T09  C~90Hj      
2015 07  20.48027  22 17 30.86   +02 16 42.7   23.2i 15OB203   T09  C~90Hj      
2016 07  05.43227  22 25 47.43   +02 41 19.1   23.5i 15OB203   T09  C~90Hj      
2016 07  05.44312  22 25 47.40   +02 41 19.1   23.4i 15OB203   T09  C~90Hj      
2016 07  05.47311  22 25 47.32   +02 41 19.1   23.4i 15OB203   T09  C~90Hj      
2016 07  05.50025  22 25 47.27   +02 41 19.1   23.3i 15OB203   T09  C~90Hj      
2016 07  07.43889  22 25 42.54   +02 41 15.1   24.1g 15OB203   T09  C~90Hj      
2016 07  07.46004  22 25 42.48   +02 41 15.1   24.1g 15OB203   T09  C~90Hj      
2016 07  07.46850  22 25 42.46   +02 41 15.1   24.1g 15OB203   T09  C~90Hj      
2016 07  12.40449  22 25 29.15   +02 40 54.1   23.2z 15OB203   T09  C~90Hj      
2016 07  12.40719  22 25 29.14   +02 40 54.1   23.5z 15OB203   T09  C~90Hj      
2016 07  12.42606  22 25 29.10   +02 40 54.1   23.9z 15OB203   T09  C~90Hj      
2016 07  12.42876  22 25 29.08   +02 40 54.1   23.7z 15OB203   T09  C~90Hj      
2016 07  12.43146  22 25 29.08   +02 40 54.1   23.0z 15OB203   T09  C~90Hj      
2016 07  12.43416  22 25 29.06   +02 40 54.1   23.3z 15OB203   T09  C~90Hj      
2016 07  12.43955  22 25 29.06   +02 40 54.0   23.4z 15OB203   T09  C~90Hj      

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     0.07       0.00    -0.07
     2   0.0000     -0.56    -0.01       0.22     0.03
     3   0.0001     -1.15     0.11       0.35    -0.03
     4   0.0001     -2.06    -0.20       0.49    -0.04
     5   0.0219   -383.35    -0.00      79.56     0.05
     6   0.0220   -384.12     0.09      79.65    -0.02
     7   0.0220   -385.45    -0.07      79.96     0.09
     8   0.9829   7082.45     0.02   -1273.20    -0.06
     9   0.9829   7082.03    -0.02   -1273.04    -0.03
    10   0.9830   7080.91    -0.11   -1272.60     0.05
    11   0.9831   7080.21     0.13   -1272.33    -0.01
    12   0.9884   7012.71     0.00   -1250.12    -0.09
    13   0.9885   7011.87    -0.05   -1249.79    -0.01
    14   0.9885   7011.59    -0.02   -1249.68     0.00
    15   1.0020   6818.06    -0.09   -1196.25    -0.05
    16   1.0020   6817.92    -0.12   -1196.19    -0.02
    17   1.0020   6817.37     0.14   -1195.97    -0.01
    18   1.0021   6817.09    -0.02   -1195.86     0.07
    19   1.0021   6817.09     0.09   -1195.86     0.05
    20   1.0021   6816.81    -0.07   -1195.75     0.13
    21   1.0021   6816.77     0.13   -1195.85    -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.

15OB203    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