Orbit Fit and Astrometric record for 13SB101

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: 13SB101   
# Created Mon Dec 18 02:37:57 2017
# Orbit generated from Bernstein formalism
# Fitting   39 observations of   39
# Arc:   3.97y
# First observation: 2013/08/05
#  Last observation: 2017/07/24
Preliminary a, adot, b, bdot, g, gdot:
  -0.000094   0.027529  -0.000003  -0.000172   0.025992   0.000000
# Chi-squared of fit:    15.65 DOF:   72 RMS:  0.11
# Min/Max residuals:    -0.29    0.30
# Exact a, adot, b, bdot, g, gdot:
  1.666411E-05  2.736457E-02  6.827998E-09 -1.710262E-04  2.592166E-02 -7.923744E-04
# Covariance matrix:
  1.2665E-13 -3.7153E-15  1.2568E-15 -6.8590E-16  1.0023E-13  3.3087E-13
 -3.7153E-15  1.6307E-13  1.3517E-15 -1.3450E-15  1.0194E-13  1.7721E-12
  1.2568E-15  1.3517E-15  6.2073E-14 -3.3547E-14  2.3623E-15  1.8433E-14
 -6.8590E-16 -1.3450E-15 -3.3547E-14  4.5152E-14 -1.6139E-15 -1.9501E-14
  1.0023E-13  1.0194E-13  2.3623E-15 -1.6139E-15  1.8527E-13  1.3790E-12
  3.3087E-13  1.7721E-12  1.8433E-14 -1.9501E-14  1.3790E-12  2.6869E-11
#      lat0       lon0       xBary       yBary       zBary        JD0
   -2.053334   11.487258    0.866887   -0.018978   -0.530116  2456510.001708
# Heliocentric elements and errors
Epoch:              2456510.5000  =  2013/08/06
Mean Anomaly:          336.45916 +/-     0.068
Argument of Peri:      288.50515 +/-     0.090
Long of Asc Node:      111.50465 +/-     0.012
Inclination:             2.06478 +/-     0.000
Eccentricity:         0.11819957 +/-    0.0001
Semi-Major Axis:     43.74202916 +/-    0.0030
Time of Perihelion: 2463420.3132 +/-      20.0
Perihelion:          38.57174030 +/-    0.0054
Aphelion:            48.91231801 +/-    0.0058
Period (y)              289.3054 +/-      0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           38.47302198 +/-    0.0006
Ecliptic Y            6.93708555 +/-    0.0001
Ecliptic Z           -1.38218861 +/-    0.0000
Ecliptic XDOT        -0.00066441 +/-    0.0000
Ecliptic YDOT         0.00281472 +/-    0.0000
Ecliptic ZDOT        -0.00001491 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   39.11786064 +/-    0.0006
Geocenter to KBO     38.57777609 +/-    0.0006
# Hcoef:  8.26

The following table shows the complete astrometric record for 13SB101. 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 (13SB101) followed by the observatory code and reference code for the source of the astrometry.

2013 08  05.50093  00 45 27.660  +02 39 12.09  24.0r 13SB101   568  C~2NKO      
2013 08  05.55416  00 45 27.548  +02 39 11.42  23.9r 13SB101   568  C~2NKO      
2013 08  31.56492  00 44 11.807  +02 30 02.31  23.8r 13SB101   568  C~2NKO      
2013 09  01.45046  00 44 08.466  +02 29 39.01  24.6r 13SB101   568  C~2NKO      
2013 09  01.48940  00 44 08.319  +02 29 38.11  24.2r 13SB101   568  C~2NKO      
2013 09  01.49828  00 44 08.273  +02 29 37.83  24.2r 13SB101   568  C~2NKO      
2013 09  05.42994  00 43 52.849  +02 27 52.40  24.6r 13SB101   568  C~2NKO      
2013 09  05.46880  00 43 52.716  +02 27 51.41  24.0r 13SB101   568  C~2NKO      
2013 09  29.36094  00 42 06.300  +02 16 07.81  24.3r 13SB101   568  C~2NKO      
2013 09  29.39977  00 42 06.102  +02 16 06.64  24.1r 13SB101   568  C~2NKO      
2013 09  29.44359  00 42 05.896  +02 16 05.34  24.1r 13SB101   568  C~2NKO      
2013 09  29.44819  00 42 05.884  +02 16 05.19  24.0r 13SB101   568  C~2NKO      
2013 09  29.45297  00 42 05.846  +02 16 05.35  24.0r 13SB101   568  C~2NKO      
2013 09  29.45785  00 42 05.821  +02 16 05.06  24.0r 13SB101   568  C~2NKO      
2013 09  29.46414  00 42 05.796  +02 16 04.77  23.2r 13SB101   568  C~2NKO      
2013 09  29.46913  00 42 05.764  +02 16 04.97  23.9r 13SB101   568  C~2NKO      
2013 09  29.50184  00 42 05.602  +02 16 03.59  23.8r 13SB101   568  C~2NKO      
2013 10  05.35958  00 41 37.815  +02 13 05.58  23.9r 13SB101   568  C~2NKO      
2013 10  06.43244  00 41 32.695  +02 12 32.94  24.1r 13SB101   568  C~2NKO      
2013 10  07.35479  00 41 28.341  +02 12 05.43  23.7r 13SB101   568  C~2NKO      
2013 10  09.49249  00 41 18.179  +02 11 01.27  23.9r 13SB101   568  C~2NKO      
2013 11  27.29243  00 38 11.285  +01 52 31.59  24.3r 13SB101   568  C~2NKO      
2013 11  27.33867  00 38 11.182  +01 52 30.90  24.1r 13SB101   568  C~2NKO      
2013 12  05.24094  00 37 55.552  +01 51 15.05  23.9r 13SB101   568  C~2NKO      
2014 07  23.57540  00 51 32.042  +03 17 45.92        13SB101   568  C~2NKO      
2014 07  27.55602  00 51 28.776  +03 17 11.71  23.6r 13SB101   568  C~2NKO      
2014 08  24.49767  00 50 28.083  +03 09 25.93  24.1r 13SB101   568  C~2NKO      
2014 08  28.46980  00 50 14.712  +03 07 52.22  23.9r 13SB101   568  C~2NKO      
2014 10  23.32666  00 46 06.816  +02 41 06.20  23.6r 13SB101   568  C~2NKO      
2014 10  27.29329  00 45 49.189  +02 39 19.17  23.9r 13SB101   568  C~2NKO      
2014 11  24.27113  00 44 07.366  +02 29 30.51  24.4r 13SB101   568  C~2NKO      
2014 11  25.29743  00 44 04.602  +02 29 16.08  24.1r 13SB101   568  C~2NKO      
2015 01  17.25388  00 43 53.491  +02 31 00.07  24.3r 13SB101   568  C~2NKO      
2015 08  20.51481  00 56 31.796  +03 47 13.66  24.1r 13SB101   568  C~2NKO      
2015 10  12.27435  00 52 52.158  +03 23 05.30  23.7r 13SB101   568  C~2NKO      
2015 10  12.35600  00 52 51.764  +03 23 02.84  24.0r 13SB101   568  C~2NKO      
2015 12  07.39898  00 49 26.646  +03 03 16.29  24.3w 13SB101   568  C~2NKO      
2015 12  31.22795  00 49 11.243  +03 02 59.48  24.6w 13SB101   568  C~2NKO      
2017 07  24.58173  01 08 55.790  +05 04 51.51  24.2w 13SB101   568  C~2NKO      

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     0.01       0.00    -0.02
  2   0.0001     -1.81    -0.00       0.04     0.14
  3   0.0714  -1261.09    -0.11     -62.49     0.19
  4   0.0738  -1316.28    -0.06     -64.39     0.00
  5   0.0739  -1318.66     0.05     -64.36     0.08
  6   0.0739  -1319.41    -0.12     -64.34     0.11
  7   0.0847  -1573.38    -0.13     -71.14     0.20
  8   0.0848  -1575.60     0.27     -71.28     0.11
  9   0.1502  -3318.87     0.10     -95.92    -0.21
 10   0.1503  -3322.06    -0.05     -95.83    -0.13
 11   0.1504  -3325.41     0.04     -95.82    -0.13
 12   0.1504  -3325.63     0.18     -95.89    -0.20
 13   0.1505  -3326.10     0.09     -95.52     0.17
 14   0.1505  -3326.55     0.01     -95.64     0.05
 15   0.1505  -3327.01     0.05     -95.76    -0.07
 16   0.1505  -3327.38     0.08     -95.39     0.30
 17   0.1506  -3330.15    -0.13     -95.71    -0.03
 18   0.1666  -3783.22     0.08     -96.78    -0.02
 19   0.1696  -3866.64    -0.19     -96.83    -0.14
 20   0.1721  -3937.49     0.19     -96.64     0.01
 21   0.1779  -4102.83    -0.06     -96.15     0.04
 22   0.3115  -7117.60    -0.11     -21.49    -0.05
 23   0.3117  -7119.29    -0.05     -21.52    -0.22
 24   0.3333  -7364.91    -0.11       0.40     0.04
 25   0.9639   5930.14    -0.29       4.32     0.04
 26   0.9748   5871.73     0.11      -8.17    -0.07
 27   1.0513   4852.48     0.03     -83.61    -0.05
 28   1.0622   4631.42    -0.00     -91.98     0.05
 29   1.2151    584.73     0.05    -123.85    -0.04
 30   1.2260    299.78     0.04    -119.35    -0.02
 31   1.3026  -1334.78     0.07     -65.78    -0.26
 32   1.3054  -1378.55    -0.07     -62.89     0.01
 33   1.4504  -1491.23     0.00      97.87    -0.06
 34   2.0397  10760.23    -0.05    -109.65     0.02
 35   2.1842   7160.87     0.05    -167.98     0.02
 36   2.1844   7154.47     0.05    -167.95    -0.03
 37   2.3378   3860.53    -0.01     -65.82     0.06
 38   2.4031   3641.41    -0.02       8.56     0.06
 39   3.9674  22905.85     0.00    -106.28     0.07

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.

13SB101    quality flag:3

Type:         7:4EEE    7:4EEE    7:4EEE

axisobj        43.987    43.995    43.979
ecceobj         0.122     0.122     0.122
incobj          2.064     2.064     2.064
qmin           38.062    38.076    38.046
qmax           49.803    49.771    49.856
amean          43.727    43.727    43.726
amin           43.314    43.331    43.302
amax           44.186    44.173    44.194
emean           0.115     0.114     0.115
emin            0.102     0.102     0.103
emax            0.127     0.127     0.128
imean           1.133     1.098     1.109
imin            0.174     0.171     0.152
imax            1.848     1.843     1.771
excite_mean     0.117     0.116     0.117
fracstop        1.000     1.000     1.000
cjmean          3.082     3.082     3.082

libcent 0       181.7     178.6     179.1
libamp  0       110.7     108.9     116.7
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       175.7     161.3     201.3
kozaiamp        180.0     180.0     178.7