Orbit Fit and Astrometric record for 14TK115

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: 14TK115   
# Created Tue Apr 14 01:10:17 2026
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     22 observations of     22
# Arc:  12.08y
# First observation: 2013/11/22
#  Last observation: 2025/12/21
# Chi-squared of fit:     9.37 DOF:     38 RMS:  0.12
# Min/Max residuals:    -0.40    0.27
# Exact a, adot, b, bdot, g, gdot:
  1.919155E-05  3.927293E-02 -3.554558E-06 -8.041657E-03  3.264148E-02  3.498959E-03
# Covariance matrix:
  3.8613E-13 -1.7857E-13 -5.7090E-14  3.3078E-14  3.6132E-14 -3.1886E-13
 -1.7857E-13  1.5783E-13  5.3657E-14 -3.2499E-14 -1.7209E-13  3.2238E-13
 -5.7090E-14  5.3657E-14  1.6391E-13 -3.1411E-14 -5.7835E-14  1.1294E-13
  3.3078E-14 -3.2499E-14 -3.1411E-14  1.1975E-14  3.7824E-14 -6.8715E-14
  3.6132E-14 -1.7209E-13 -5.7835E-14  3.7824E-14  4.5910E-13 -3.9242E-13
 -3.1886E-13  3.2238E-13  1.1294E-13 -6.8715E-14 -3.9242E-13  6.8352E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
   -3.365992   13.218358   -0.714818   -0.039738   -0.678030  2456618.639868
# Heliocentric elements and errors
Epoch:              2456618.5000  =  2013/11/22
Mean Anomaly:           21.06573 +/-     0.006
Argument of Peri:      162.18528 +/-     0.007
Long of Asc Node:      178.81449 +/-     0.000
Inclination:            11.98805 +/-     0.000
Eccentricity:         0.23043773 +/-    0.0001
Semi-Major Axis:     39.40774207 +/-    0.0055
Time of Perihelion: 2451331.0681 +/-       1.9
Perihelion:          30.32671128 +/-    0.0056
Aphelion:            48.48877286 +/-    0.0077
Period (y)              247.3891 +/-      0.05
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           30.26959848 +/-    0.0006
Ecliptic Y            7.84731536 +/-    0.0001
Ecliptic Z           -1.79891153 +/-    0.0000
Ecliptic XDOT        -0.00051273 +/-    0.0000
Ecliptic YDOT         0.00326287 +/-    0.0000
Ecliptic ZDOT        -0.00069043 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   31.32189398 +/-    0.0006
Geocenter to KBO     30.63585372 +/-    0.0006
# Hcoef:  8.24

The following table shows the complete astrometric record for 14TK115. 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 (14TK115) followed by the observatory code and reference code for the source of the astrometry.

2013 11  22.13909  00 53 52.939  +02 06 59.30  22.7i 14TK115   W84  C~52UG      
2013 11  22.15022  00 53 52.899  +02 06 59.16  22.7z 14TK115   W84  C~52UG      
2014 10  02.29411  01 07 15.868  +03 02 43.72  24.1g 14TK115   W84  C~52UG      
2014 11  14.07483  01 03 25.994  +02 37 00.69  23.4r 14TK115   W84  C~52UG      
2014 11  14.07621  01 03 25.993  +02 37 00.74  23.0i 14TK115   W84  C~52UG      
2015 11  07.11042  01 12 56.923  +03 06 41.02  23.0r 14TK115   W84  C~52UG      
2015 11  07.11179  01 12 56.918  +03 06 41.04  23.2i 14TK115   W84  C~52UG      
2015 11  07.11317  01 12 56.908  +03 06 40.94  23.7g 14TK115   W84  C~52UG      
2016 10  23.21561  01 23 06.542  +03 40 22.32  22.8r 14TK115   W84  C~52UG      
2016 10  23.21697  01 23 06.543  +03 40 22.23  23.8g 14TK115   W84  C~52UG      
2016 10  29.19725  01 22 33.103  +03 36 47.67  24.4g 14TK115   W84  C~52UG      
2016 11  05.15757  01 21 55.613  +03 32 53.83  22.8r 14TK115   W84  C~52UG      
2016 11  05.15895  01 21 55.610  +03 32 53.66  22.7i 14TK115   W84  C~52UG      
2017 08  27.37486  01 36 32.605  +04 40 12.43  23.4i 14TK115   W84  C~52UG      
2017 08  27.38869  01 36 32.555  +04 40 12.23  23.4r 14TK115   W84  C~52UG      
2017 08  27.39145  01 36 32.548  +04 40 12.07  22.6z 14TK115   W84  C~52UG      
2018 09  11.36127  01 44 19.661  +04 56 05.37  22.7i 14TK115   W84  C~52UG      
2018 09  11.36265  01 44 19.656  +04 56 05.16  23.7r 14TK115   W84  C~52UG      
2018 10  20.17485  01 40 59.628  +04 31 51.37  22.7z 14TK115   W84  C~52UG      
2025 12  21.12236  02 34 33.998  +06 39 33.48  23.7G 14TK115   G37              
2025 12  21.17052  02 34 33.832  +06 39 33.06        14TK115   G37              
2025 12  21.21847  02 34 33.673  +06 39 32.83        14TK115   G37              

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    -0.00       0.00    -0.08
     2   0.0000      0.00     0.00       0.00     0.02
     3   0.8601      0.00    -0.03       0.00    -0.18
     4   0.9772      0.00     0.01       0.00    -0.07
     5   0.9772      0.00     0.09       0.00     0.02
     6   1.9575      0.00     0.00       0.00     0.02
     7   1.9575      0.00     0.03       0.00     0.08
     8   1.9575      0.00    -0.01       0.00     0.02
     9   2.9188      0.00    -0.15       0.00     0.04
    10   2.9188      0.00    -0.02       0.00     0.00
    11   2.9351      0.00     0.09       0.00     0.27
    12   2.9542      0.00    -0.06       0.00     0.15
    13   2.9542      0.00     0.01       0.00     0.02
    14   3.7625      0.00     0.11       0.00    -0.13
    15   3.7625      0.00    -0.00       0.00     0.08
    16   3.7625      0.00     0.02       0.00     0.00
    17   4.8028      0.00    -0.02       0.00     0.17
    18   4.8028      0.00    -0.01       0.00     0.01
    19   4.9091      0.00     0.05       0.00    -0.40
    20  12.0794      0.00     0.10       0.00     0.21
    21  12.0795      0.00     0.10       0.00     0.14
    22  12.0796      0.00     0.18       0.00     0.25

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.

14TK115    quality flag:3

Type:           3:2E      3:2E      3:2E

axisobj        39.666    39.667    39.666
ecceobj         0.236     0.236     0.236
incobj         11.958    11.958    11.958
qmin           28.754    28.755    28.754
qmax           50.797    50.798    50.796
amean          39.456    39.456    39.456
amin           38.954    38.952    38.956
amax           40.060    40.064    40.055
emean           0.230     0.230     0.230
emin            0.196     0.196     0.196
emax            0.270     0.270     0.270
imean          11.862    11.862    11.862
imin            9.914     9.914     9.914
imax           13.579    13.579    13.580
excite_mean     0.309     0.309     0.309
fracstop        1.000     1.000     1.000
cjmean          2.943     2.943     2.943

libcent 0       179.6     179.6     179.6
libamp  0       109.4     109.3     109.4
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        95.7      95.7      95.7
kozaiamp         60.1      60.1      60.1