Orbit Fit and Astrometric record for 13GO137

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: 13GO137   
# Created Fri Apr 26 01:14:31 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     36 observations of     36
# Arc:   8.32y
# First observation: 2013/02/08
#  Last observation: 2021/06/07
# Chi-squared of fit:    24.98 DOF:     66 RMS:  0.15
# Min/Max residuals:    -0.49    0.40
# Exact a, adot, b, bdot, g, gdot:
  1.507622E-05  1.944248E-02 -8.628654E-06 -1.086053E-02  2.357266E-02 -1.479382E-03
# Covariance matrix:
  1.8929E-13 -6.5381E-14 -3.1275E-14  4.3847E-14  1.0637E-13 -4.6617E-13
 -6.5381E-14  9.3499E-14  3.9811E-14 -5.8724E-14  1.4775E-14  6.3327E-13
 -3.1275E-14  3.9811E-14  7.8531E-14 -4.3748E-14 -6.8101E-16  3.1207E-13
  4.3847E-14 -5.8724E-14 -4.3748E-14  5.3928E-14 -1.6534E-15 -4.5858E-13
  1.0637E-13  1.4775E-14 -6.8101E-16 -1.6534E-15  1.3691E-13  2.5581E-14
 -4.6617E-13  6.3327E-13  3.1207E-13 -4.5858E-13  2.5581E-14  4.9402E-12
#      lat0       lon0       xBary       yBary       zBary        JD0
    1.921503 -146.743504    0.944420    0.009530   -0.282467  2456332.057178
# Heliocentric elements and errors
Epoch:              2456332.5000  =  2013/02/09
Mean Anomaly:          253.27821 +/-     0.034
Argument of Peri:      292.33970 +/-     0.027
Long of Asc Node:       35.39151 +/-     0.000
Inclination:            29.29477 +/-     0.000
Eccentricity:         0.08994782 +/-    0.0001
Semi-Major Axis:     41.34853541 +/-    0.0025
Time of Perihelion: 2485122.3392 +/-      11.0
Perihelion:          37.62932478 +/-    0.0047
Aphelion:            45.06774605 +/-    0.0049
Period (y)              265.8878 +/-      0.02
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -36.20722786 +/-    0.0006
Ecliptic Y          -22.61393449 +/-    0.0004
Ecliptic Z            1.42204918 +/-    0.0000
Ecliptic XDOT         0.00134037 +/-    0.0000
Ecliptic YDOT        -0.00181639 +/-    0.0000
Ecliptic ZDOT        -0.00126632 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   42.71276305 +/-    0.0005
Geocenter to KBO     42.42208335 +/-    0.0007
# Hcoef:  7.20

The following table shows the complete astrometric record for 13GO137. 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 (13GO137) followed by the observatory code and reference code for the source of the astrometry.

2013 02  08.55640  14 06 48.224  -10 47 32.46  23.6r 13GO137   568  C~1XRY      
2013 02  08.60359  14 06 48.226  -10 47 32.57  23.0r 13GO137   568  C~1XRY      
2013 04  04.41383  14 04 04.513  -10 37 07.53  23.4r 13GO137   568  C~1XRY      
2013 04  04.45396  14 04 04.332  -10 37 06.84  23.4r 13GO137   568  C~1XRY      
2013 04  04.49439  14 04 04.141  -10 37 06.03  23.6r 13GO137   568  C~1XRY      
2013 04  05.53143  14 03 59.427  -10 36 46.59  22.9r 13GO137   568  C~1XRY      
2013 04  05.53531  14 03 59.405  -10 36 46.52  23.5r 13GO137   568  C~1XRY      
2013 04  06.58684  14 03 54.555  -10 36 26.64  23.7r 13GO137   568  C~1XRY      
2013 04  08.38751  14 03 46.244  -10 35 52.72  23.6r 13GO137   568  C~1XRY      
2013 05  11.41804  14 01 09.381  -10 25 30.97  23.6r 13GO137   568  C~1XRY      
2013 05  12.41931  14 01 04.841  -10 25 14.02  23.6r 13GO137   568  C~1XRY      
2013 06  13.25755  13 59 04.294  -10 18 40.68  23.7r 13GO137   568  C~1XRY      
2013 06  13.29820  13 59 04.170  -10 18 40.33  23.8r 13GO137   568  C~1XRY      
2013 07  04.27893  13 58 21.320  -10 17 52.83  23.6r 13GO137   568  C~1XRY      
2013 07  06.28622  13 58 19.093  -10 17 58.68  23.7r 13GO137   568  C~1XRY      
2014 02  25.51607  14 09 47.968  -11 44 22.76  23.5r 13GO137   568  C~1XRY      
2014 02  25.55969  14 09 47.866  -11 44 22.43  23.6r 13GO137   568  C~1XRY      
2014 02  25.60433  14 09 47.754  -11 44 22.14  23.6r 13GO137   568  C~1XRY      
2014 03  26.51083  14 08 12.280  -11 38 32.83        13GO137   568  C~1XRY      
2014 03  27.41673  14 08 08.523  -11 38 18.08  23.4r 13GO137   568  C~1XRY      
2014 03  28.41797  14 08 04.273  -11 38 01.42  23.4r 13GO137   568  C~1XRY      
2014 03  28.45726  14 08 04.104  -11 38 00.83  23.6r 13GO137   568  C~1XRY      
2014 04  05.38215  14 07 29.079  -11 35 42.89  23.1r 13GO137   568  C~1XRY      
2014 04  29.33527  14 05 34.725  -11 28 11.44  23.1r 13GO137   568  C~1XRY      
2014 04  29.41097  14 05 34.349  -11 28 09.88  23.6r 13GO137   568  C~1XRY      
2014 04  29.41601  14 05 34.328  -11 28 09.86  23.4r 13GO137   568  C~1XRY      
2014 05  22.40174  14 03 48.898  -11 21 33.13  23.5r 13GO137   568  C~1XRY      
2014 05  22.40562  14 03 48.880  -11 21 33.12  23.4r 13GO137   568  C~1XRY      
2014 05  28.37385  14 03 24.587  -11 20 08.51  23.5r 13GO137   568  C~1XRY      
2014 05  28.37773  14 03 24.564  -11 20 08.39  23.6r 13GO137   568  C~1XRY      
2015 01  26.65311  14 13 42.486  -12 41 58.53  23.7r 13GO137   568  C~1XRY      
2015 04  27.34173  14 09 15.795  -12 27 57.62  23.2r 13GO137   568  C~2KOG      
2015 04  27.35111  14 09 15.732  -12 27 57.99  24.6u 13GO137   568  C~2KOG      
2015 04  27.40797  14 09 15.466  -12 27 56.35  23.3r 13GO137   568  C~2KOG      
2021 06  06.97024  14 28 02.55   -18 11 43.00        13GO137   W84  C~7xNS      
2021 06  07.12201  14 28 01.95   -18 11 40.60        13GO137   W84  C~7xNS      

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    -0.31       0.00     0.40
     2   0.0001      0.00     0.39       0.00     0.25
     3   0.1502      0.00     0.03       0.00    -0.04
     4   0.1503      0.00     0.09       0.00    -0.10
     5   0.1504      0.00     0.03       0.00    -0.04
     6   0.1533      0.00     0.27       0.00     0.04
     7   0.1533      0.00     0.21       0.00     0.03
     8   0.1561      0.00    -0.11       0.00     0.15
     9   0.1611      0.00    -0.02       0.00    -0.03
    10   0.2515      0.00     0.15       0.00     0.03
    11   0.2542      0.00     0.17       0.00     0.01
    12   0.3414      0.00     0.02       0.00    -0.04
    13   0.3415      0.00    -0.05       0.00     0.04
    14   0.3990      0.00     0.01       0.00    -0.14
    15   0.4045      0.00     0.10       0.00    -0.12
    16   1.0457      0.00     0.11       0.00    -0.11
    17   1.0459      0.00     0.10       0.00    -0.08
    18   1.0460      0.00    -0.01       0.00    -0.10
    19   1.1251      0.00    -0.45       0.00     0.03
    20   1.1276      0.00     0.05       0.00    -0.05
    21   1.1304      0.00    -0.07       0.00     0.01
    22   1.1305      0.00    -0.05       0.00    -0.05
    23   1.1522      0.00    -0.18       0.00    -0.05
    24   1.2177      0.00    -0.02       0.00    -0.06
    25   1.2179      0.00    -0.08       0.00     0.08
    26   1.2180      0.00    -0.02       0.00     0.01
    27   1.2809      0.00     0.01       0.00     0.07
    28   1.2809      0.00    -0.01       0.00     0.02
    29   1.2972      0.00    -0.14       0.00    -0.05
    30   1.2973      0.00    -0.25       0.00     0.02
    31   1.9633      0.00     0.16       0.00     0.07
    32   2.2116      0.00     0.01       0.00     0.06
    33   2.2116      0.00    -0.24       0.00    -0.49
    34   2.2118      0.00     0.00       0.00     0.09
    35   8.3242      0.00     0.02       0.00     0.00
    36   8.3246      0.00     0.13       0.00     0.13

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.

13GO137    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        41.231    41.231    41.231
ecceobj         0.093     0.093     0.093
incobj         29.344    29.344    29.344
qmin           37.124    37.137    37.171
qmax           46.041    46.040    46.070
amean          41.483    41.483    41.484
amin           41.168    41.157    41.174
amax           41.822    41.824    41.836
emean           0.088     0.088     0.088
emin            0.076     0.075     0.076
emax            0.102     0.101     0.101
imean          28.624    28.623    28.624
imin           28.247    28.248    28.256
imax           28.924    28.923    28.925
excite_mean     0.487     0.487     0.487
fracstop        1.000     1.000     1.000
cjmean          2.778     2.778     2.778

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       182.1     182.2     181.5
kozaiamp        180.0     180.0     180.0