Orbit Fit and Astrometric record for 15OD203

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: 15OD203   
# Created Tue Sep  2 01:10:50 2025
# Orbit generated from Bernstein formalism
# Fitting     20 observations of     20
# Arc:   0.84y
# First observation: 2014/09/18
#  Last observation: 2015/07/22
Preliminary a, adot, b, bdot, g, gdot:
  -0.000027   0.027401  -0.000001  -0.004447   0.024184   0.000000
# Chi-squared of fit:     9.13 DOF:     34 RMS:  0.12
# Min/Max residuals:    -0.22    0.28
# Exact a, adot, b, bdot, g, gdot:
  1.708127E-05  2.656742E-02 -2.497343E-06 -4.415207E-03  2.472407E-02 -8.371324E-03
# Covariance matrix:
  5.2487E-13  3.7097E-11  6.7378E-14 -4.7562E-12  1.4506E-11  1.1773E-09
  3.7097E-11  6.1418E-09  9.5795E-12 -7.4280E-10  1.9221E-09  1.8163E-07
  6.7378E-14  9.5795E-12  2.0224E-13 -1.4036E-12  3.2302E-12  2.8935E-10
 -4.7562E-12 -7.4280E-10 -1.4036E-12  9.0815E-11 -2.3861E-10 -2.2127E-08
  1.4506E-11  1.9221E-09  3.2302E-12 -2.3861E-10  6.7313E-10  5.8707E-08
  1.1773E-09  1.8163E-07  2.8935E-10 -2.2127E-08  5.8707E-08  5.4199E-06
#      lat0       lon0       xBary       yBary       zBary        JD0
    9.496236  -24.138216   -0.329820    0.157140   -0.938841  2456918.735968
# Heliocentric elements and errors
Epoch:              2456910.5000  =  2014/09/10
Mean Anomaly:          338.53260 +/-     3.462
Argument of Peri:      192.44427 +/-     7.726
Long of Asc Node:      200.06837 +/-     0.059
Inclination:            13.29497 +/-     0.014
Eccentricity:         0.45003589 +/-    0.0896
Semi-Major Axis:     64.62628533 +/-    6.5171
Time of Perihelion: 2468226.4004 +/-     633.2
Perihelion:          35.54213728 +/-    6.8104
Aphelion:            93.71043337 +/-   11.0833
Period (y)              519.5436 +/-     78.59
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           37.40550348 +/-    0.0382
Ecliptic Y          -16.39976098 +/-    0.0171
Ecliptic Z            6.67289477 +/-    0.0070
Ecliptic XDOT         0.00043765 +/-    0.0002
Ecliptic YDOT         0.00302111 +/-    0.0001
Ecliptic ZDOT        -0.00063505 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   41.38419234 +/-    0.0352
Geocenter to KBO     40.44641199 +/-    0.0424
# Hcoef:  8.96

The following table shows the complete astrometric record for 15OD203. 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 (15OD203) followed by the observatory code and reference code for the source of the astrometry.

2014 09  18.23519  22 16 40.88   -00 31 10.6   26.9g 15OD203   T09  C~90Hj      
2014 09  18.26405  22 16 40.77   -00 31 11.5   26.6g 15OD203   T09  C~90Hj      
2014 09  18.27477  22 16 40.72   -00 31 11.8   26.0g 15OD203   T09  C~90Hj      
2014 09  22.22908  22 16 25.28   -00 33 15.2   25.2r 15OD203   T09  C~90Hj      
2014 09  22.25775  22 16 25.16   -00 33 16.6   25.1r 15OD203   T09  C~90Hj      
2014 09  22.26849  22 16 25.12   -00 33 16.7   25.4r 15OD203   T09  C~90Hj      
2014 09  22.34435  22 16 24.82   -00 33 19.1   24.6i 15OD203   T09  C~90Hj      
2014 09  22.36694  22 16 24.74   -00 33 19.9   24.3i 15OD203   T09  C~90Hj      
2015 07  15.44387  22 27 09.07   +00 13 27.0   25.3r 15OD203   T09  C~90Hj      
2015 07  15.48044  22 27 08.97   +00 13 26.8   25.6r 15OD203   T09  C~90Hj      
2015 07  15.48467  22 27 08.95   +00 13 26.8   24.8r 15OD203   T09  C~90Hj      
2015 07  15.50409  22 27 08.89   +00 13 26.5   25.1r 15OD203   T09  C~90Hj      
2015 07  20.44763  22 26 53.50   +00 12 31.4   24.9i 15OD203   T09  C~90Hj      
2015 07  20.46669  22 26 53.46   +00 12 31.0   24.7i 15OD203   T09  C~90Hj      
2015 07  20.51051  22 26 53.30   +00 12 30.7   24.3i 15OD203   T09  C~90Hj      
2015 07  22.42737  22 26 46.95   +00 12 05.9   24.3z 15OD203   T09  C~90Hj      
2015 07  22.44630  22 26 46.89   +00 12 05.3   25.0z 15OD203   T09  C~90Hj      
2015 07  22.44899  22 26 46.86   +00 12 05.3   24.6z 15OD203   T09  C~90Hj      
2015 07  22.46793  22 26 46.79   +00 12 05.2   24.3z 15OD203   T09  C~90Hj      
2015 07  22.51384  22 26 46.64   +00 12 04.3   24.2z 15OD203   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    -0.02       0.00    -0.07
     2   0.0001     -1.86     0.08      -0.24    -0.10
     3   0.0001     -2.67    -0.00      -0.25    -0.03
     4   0.0109   -263.26     0.17     -31.16     0.28
     5   0.0110   -265.44    -0.13     -31.81    -0.14
     6   0.0110   -266.04    -0.02     -31.69     0.07
     7   0.0113   -271.10    -0.08     -32.29     0.07
     8   0.0113   -272.51    -0.00     -32.60    -0.06
     9   0.8219   9759.21    -0.13    -927.37    -0.12
    10   0.8220   9757.74     0.08    -927.01    -0.03
    11   0.8220   9757.46    -0.00    -926.90     0.05
    12   0.8221   9756.51    -0.06    -926.85    -0.05
    13   0.8356   9520.89    -0.09    -894.31     0.06
    14   0.8357   9520.19     0.18    -894.46    -0.22
    15   0.8358   9517.84     0.08    -893.87     0.08
    16   0.8410   9419.88     0.19    -882.37     0.23
    17   0.8411   9418.82     0.14    -882.60    -0.12
    18   0.8411   9418.40    -0.14    -882.44     0.03
    19   0.8412   9417.38    -0.14    -882.15     0.20
    20   0.8413   9414.95    -0.12    -882.17    -0.11

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.

15OD203    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