Orbit Fit and Astrometric record for 14OG392

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: 14OG392   
# Created Thu Dec 14 02:38:03 2017
# Orbit generated from Bernstein formalism
# Fitting   36 observations of   36
# Arc:   4.25y
# First observation: 2013/07/12
#  Last observation: 2017/10/11
Preliminary a, adot, b, bdot, g, gdot:
  -0.018094   0.195865   0.006365  -0.033830   0.027465   0.000000
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# WARNING Fitting with energy constraint
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# Chi-squared of fit:  9999.99 DOF:   67 RMS: 99.99
# Min/Max residuals: -3684.72 1577.61
# Exact a, adot, b, bdot, g, gdot:
 -7.614559E-03  1.696256E-01  2.476529E-03 -2.654590E-02  8.246210E-02 -3.337273E-02
# Covariance matrix:
  1.6267E-13 -1.2672E-13 -1.2959E-14  1.8137E-14  8.9320E-15 -1.1459E-13
 -1.2672E-13  1.7214E-13  2.3996E-14 -3.3860E-14 -8.1013E-14  2.1783E-13
 -1.2959E-14  2.3996E-14  1.0446E-13 -3.6174E-14 -2.9328E-14  4.0357E-14
  1.8137E-14 -3.3860E-14 -3.6174E-14  2.1700E-14  4.2965E-14 -5.7642E-14
  8.9320E-15 -8.1013E-14 -2.9328E-14  4.2965E-14  4.6814E-13 -2.9848E-13
 -1.1459E-13  2.1783E-13  4.0357E-14 -5.7642E-14 -2.9848E-13  3.8053E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
    2.975332  -49.905556    0.349261    0.049696   -0.955923  2456485.984908
# Heliocentric elements and errors
Epoch:              2456480.5000  =  2013/07/07
Mean Anomaly:          349.39129 +/-     0.001
Argument of Peri:      199.98247 +/-     0.002
Long of Asc Node:      146.03692 +/-     0.000
Inclination:             9.33638 +/-     0.000
Eccentricity:         0.52674934 +/-    0.0000
Semi-Major Axis:     25.62530783 +/-    0.0021
Time of Perihelion: 2457876.7467 +/-       0.1
Perihelion:          12.12719389 +/-    0.0013
Aphelion:            39.12342178 +/-    0.0033
Period (y)              129.7215 +/-      0.02
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X            8.07746915 +/-    0.0001
Ecliptic Y          -10.27723806 +/-    0.0001
Ecliptic Z            0.65950254 +/-    0.0000
Ecliptic XDOT         0.00361878 +/-    0.0000
Ecliptic YDOT         0.00443800 +/-    0.0000
Ecliptic ZDOT        -0.00093754 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   13.08824181 +/-    0.0001
Geocenter to KBO     12.12717194 +/-    0.0001
# Hcoef:  9.93

The following table shows the complete astrometric record for 14OG392. 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 (14OG392) followed by the observatory code and reference code for the source of the astrometry.

2013 07  12.48413  20 46 51.132  -14 50 53.75  21.8w 14OG392   F51  C~1vXe      
2013 07  12.48545  20 46 51.131  -14 50 53.48  21.4w 14OG392   F51  C~1vXe      
2013 07  12.49909  20 46 50.937  -14 50 54.73  21.6w 14OG392   F51  C~1vXe      
2013 07  12.50042  20 46 50.910  -14 50 54.74  21.7w 14OG392   F51  C~1vXe      
2013 07  12.51407  20 46 50.723  -14 50 55.62  21.7w 14OG392   F51  C~1vXe      
2013 07  12.51539  20 46 50.707  -14 50 55.80  21.6w 14OG392   F51  C~1vXe      
2013 07  12.52907  20 46 50.511  -14 50 56.66  21.7w 14OG392   F51  C~1vXe      
2013 07  12.53039  20 46 50.495  -14 50 56.66  21.8w 14OG392   F51  C~1vXe      
2014 07  28.49510  21 23 43.338  -13 48 03.86  21.4w 14OG392   F51  C@0615      
2014 07  28.50639  21 23 43.180  -13 48 05.03  21.4w 14OG392   F51  C@0615      
2014 07  28.51768  21 23 43.009  -13 48 05.72  21.3w 14OG392   F51  C@0615      
2014 07  29.313162 21 23 31.61   -13 49 12.1   21.3V 14OG392   H21  C~17NO      
2014 07  29.326160 21 23 31.40   -13 49 12.3   20.9V 14OG392   H21  C~17NO      
2014 07  29.339079 21 23 31.25   -13 49 12.9         14OG392   H21  C~17NO      
2015 06  25.55263  22 11 11.900  -11 17 40.95  21.6w 14OG392   F51  C~1vXe      
2015 06  25.56378  22 11 11.850  -11 17 41.29  21.5w 14OG392   F51  C~1vXe      
2015 06  25.57493  22 11 11.796  -11 17 41.80  21.6w 14OG392   F51  C~1vXe      
2015 06  25.58612  22 11 11.740  -11 17 42.34  21.4w 14OG392   F51  C~1vXe      
2015 07  12.50026  22 09 15.348  -11 33 30.75  21.5w 14OG392   F51  C~1vXe      
2015 07  12.51139  22 09 15.246  -11 33 31.51  21.5w 14OG392   F51  C~1vXe      
2015 07  12.52254  22 09 15.141  -11 33 32.30  21.6w 14OG392   F51  C~1vXe      
2015 07  12.53369  22 09 15.027  -11 33 33.10  21.5w 14OG392   F51  C~1vXe      
2015 07  14.54315  22 08 55.930  -11 35 55.04  21.4w 14OG392   F51  C~1vXe      
2015 07  14.55458  22 08 55.816  -11 35 56.24  21.4w 14OG392   F51  C~1vXe      
2015 07  14.56593  22 08 55.713  -11 35 56.87  21.4w 14OG392   F51  C~1vXe      
2015 07  14.57721  22 08 55.608  -11 35 57.76  21.4w 14OG392   F51  C~1vXe      
2016 08  28.69002  22 43 28.63   -10 23 47.9   19.6R 14OG392   D29  C~1x8l      
2016 08  28.71830  22 43 28.18   -10 23 50.2   19.7R 14OG392   D29  C~1x8l      
2017 09  15.40527  23 25 55.626  -08 02 13.82  21.1w 14OG392   F51  C~2KWy      
2017 09  15.41638  23 25 55.460  -08 02 14.99  21.1w 14OG392   F51  C~2KWy      
2017 09  15.42757  23 25 55.285  -08 02 16.21  21.2w 14OG392   F51  C~2KWy      
2017 09  15.43867  23 25 55.130  -08 02 17.54  21.6w 14OG392   F51  C~2KWy      
2017 10  11.36275  23 19 53.59   -08 45 04.3   17.9o 14OG392   T08  C~2Ma9      
2017 10  11.36997  23 19 53.52   -08 45 05.4   17.9o 14OG392   T08  C~2Ma9      
2017 10  11.37700  23 19 53.43   -08 45 05.8   17.9o 14OG392   T08  C~2Ma9      
2017 10  11.38426  23 19 53.32   -08 45 06.2   17.9o 14OG392   T08  C~2Ma9      

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  1577.31       0.00  -511.87
  2   0.0000      0.06  1577.61       0.26  -511.59
  3   0.0000     -2.99  1577.02      -0.20  -511.94
  4   0.0000     -3.37  1576.88      -0.10  -511.83
  5   0.0001     -6.21  1576.49      -0.23  -511.85
  6   0.0001     -6.49  1576.46      -0.34  -511.95
  7   0.0001     -9.45  1575.95      -0.42  -511.91
  8   0.0001     -9.68  1575.97      -0.36  -511.84
  9   1.0432  32157.38   142.02   -5576.87  -180.51
 10   1.0432  32154.77   141.64   -5577.29  -180.76
 11   1.0432  32152.13   141.23   -5577.19  -180.50
 12   1.0454  31969.43   112.97   -5589.89  -180.39
 13   1.0454  31966.38   112.50   -5589.14  -179.44
 14   1.0455  31964.06   112.74   -5589.04  -179.16
 15   1.9523  77720.76   154.44  -11027.96   148.94
 16   1.9523  77719.84   154.28  -11028.02   149.08
 17   1.9523  77718.79   153.99  -11028.23   149.06
 18   1.9524  77717.69   153.66  -11028.46   149.02
 19   1.9987  75518.02  -303.04  -11329.86   167.58
 20   1.9987  75516.13  -303.32  -11330.05   167.58
 21   1.9987  75514.18  -303.66  -11330.26   167.57
 22   1.9988  75512.08  -304.14  -11330.43   167.60
 23   2.0043  75158.02  -368.49  -11366.43   169.91
 24   2.0043  75155.77  -368.99  -11366.99   169.54
 25   2.0043  75153.91  -369.11  -11367.05   169.68
 26   2.0044  75151.93  -369.38  -11367.36   169.57
 27   3.1299 111581.57 -2719.74  -19521.80   524.29
 28   3.1300 111572.46 -2721.18  -19521.22   525.27
 29   4.1777 167532.83 -2040.77  -29444.07   525.67
 30   4.1778 167528.29 -2041.41  -29444.01   525.76
 31   4.1778 167523.50 -2042.27  -29443.92   525.86
 32   4.1778 167519.11 -2042.77  -29444.14   525.66
 33   4.2488 157839.24 -3683.40  -29340.41   601.05
 34   4.2488 157837.06 -3683.66  -29341.09   600.31
 35   4.2489 157834.85 -3684.00  -29340.79   600.55
 36   4.2489 157832.19 -3684.72  -29340.33   600.96

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.

14OG392    quality flag:3

Type:       CENTAURR  CENTAURR  CENTAURR

axisobj        12.134    12.134    12.134
ecceobj         0.185     0.185     0.185
incobj          9.042     9.042     9.042
qmin            9.544     9.797     9.745
qmax           16.296    18.526    15.787
amean          12.103    12.793    11.425
amin           11.449    10.773    10.904
amax           13.047    14.342    12.915
emean           0.195     0.201     0.117
emin            0.162     0.077     0.050
emax            0.249     0.292     0.222
imean           7.291     5.722     7.102
imin            6.464     3.759     4.028
imax            7.892     7.864     7.864
excite_mean     0.233     0.229     0.175
fracstop        0.001     0.002     0.001
cjmean          3.723     3.637     3.852

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       228.7     202.3     204.0
kozaiamp        148.8     176.4     169.1