Orbit Fit and Astrometric record for 14KL84

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: 14KL84    
# Created Thu Apr 25 01:15:48 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     20 observations of     20
# Arc:   2.01y
# First observation: 2013/04/18
#  Last observation: 2015/04/22
# Chi-squared of fit:    21.62 DOF:     34 RMS:  0.18
# Min/Max residuals:    -0.39    0.41
# Exact a, adot, b, bdot, g, gdot:
  5.034530E-05  6.564723E-01  4.564170E-06  6.142353E-02  2.027518E-01 -1.180072E-01
# Covariance matrix:
  3.5689E-13  7.5495E-13  2.3616E-16  6.8603E-13  1.1953E-12 -1.4155E-12
  7.5495E-13  1.1731E-10 -2.3385E-12  5.8594E-11 -5.5863E-12 -1.3848E-10
  2.3616E-16 -2.3385E-12  3.5576E-13 -3.3233E-12  1.2158E-12  5.3487E-12
  6.8603E-13  5.8594E-11 -3.3233E-12  8.3369E-11 -1.6894E-11 -1.1596E-10
  1.1953E-12 -5.5863E-12  1.2158E-12 -1.6894E-11  2.6336E-11  4.3964E-11
 -1.4155E-12 -1.3848E-10  5.3487E-12 -1.1596E-10  4.3964E-11  2.7943E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
   13.625342 -159.225587   -0.131096    0.234960   -0.969253  2456400.717228
# Heliocentric elements and errors
Epoch:              2456400.5000  =  2013/04/18
Mean Anomaly:          356.04618 +/-     0.000
Argument of Peri:       91.21146 +/-     0.000
Long of Asc Node:      134.55980 +/-     0.000
Inclination:            12.25440 +/-     0.000
Eccentricity:         0.64324739 +/-    0.0000
Semi-Major Axis:     16.02849832 +/-    0.0000
Time of Perihelion: 2456657.9259 +/-       0.0
Perihelion:           5.71820857 +/-    0.0000
Aphelion:            26.33878807 +/-    0.0000
Period (y)               64.1723 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           -5.36696469 +/-    0.0000
Ecliptic Y           -2.17414662 +/-    0.0000
Ecliptic Z            1.16193290 +/-    0.0000
Ecliptic XDOT         0.00476854 +/-    0.0000
Ecliptic YDOT        -0.00766944 +/-    0.0000
Ecliptic ZDOT         0.00043084 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO    5.90607976 +/-    0.0000
Geocenter to KBO      4.93221597 +/-    0.0000
# Hcoef: 13.84

The following table shows the complete astrometric record for 14KL84. 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 (14KL84) followed by the observatory code and reference code for the source of the astrometry.

2013 04  18.21645  13 37 08.07   +04 31 55.3   21.7V 14KL84    G96  C~15UA      
2013 04  18.22471  13 37 07.89   +04 31 56.3   21.1V 14KL84    G96  C~15UA      
2013 04  18.23303  13 37 07.71   +04 31 57.5   20.9V 14KL84    G96  C~15UA      
2013 04  18.24135  13 37 07.53   +04 31 59.0   21.1V 14KL84    G96  C~15UA      
2013 05  12.16061  13 29 34.32   +05 09 53.2   21.9V 14KL84    691  C~15UA      
2013 05  12.17913  13 29 34.05   +05 09 53.8   21.5V 14KL84    691  C~15UA      
2013 05  12.19765  13 29 33.73   +05 09 54.3   21.2V 14KL84    691  C~15UA      
2014 05  20.43494  15 59 11.274  -05 51 58.30  21.2r 14KL84    F51  C~157k      
2014 05  20.44718  15 59 10.995  -05 51 57.65  21.2r 14KL84    F51  C~157k      
2014 05  20.45916  15 59 10.722  -05 51 57.24  21.4r 14KL84    F51  C~157k      
2014 05  20.47120  15 59 10.419  -05 51 56.56  21.4r 14KL84    F51  C~157k      
2014 05  22.38494  15 58 27.26   -05 50 27.3   21.2R 14KL84    291  C~157k      
2014 05  22.39916  15 58 26.93   -05 50 26.5   21.1R 14KL84    291  C~157k      
2014 05  22.41069  15 58 26.67   -05 50 26.1   20.9R 14KL84    291  C~157k      
2014 05  31.37937  15 55 06.41   -05 46 01.6         14KL84    291  C~157k      
2014 05  31.40011  15 55 05.95   -05 46 01.3         14KL84    291  C~157k      
2014 06  28.22201  15 46 52.54   -06 01 56.7   21.6R 14KL84    G37  C~16Wt      
2014 06  28.28161  15 46 51.79   -06 02 01.6         14KL84    G37  C~16Wt      
2015 04  22.46398  18 23 46.15   -13 31 08.7   21.9R 14KL84    G37  C~1Rev      
2015 04  22.47689  18 23 46.15   -13 31 08.1         14KL84    G37  C~1Rev      

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     0.18       0.00    -0.02
     2   0.0000      0.00     0.12       0.00    -0.20
     3   0.0000      0.00     0.09       0.00    -0.18
     4   0.0001      0.00     0.06       0.00     0.14
     5   0.0656      0.00    -0.39       0.00     0.26
     6   0.0656      0.00     0.08       0.00     0.06
     7   0.0657      0.00    -0.19       0.00    -0.23
     8   1.0875      0.00    -0.16       0.00    -0.08
     9   1.0876      0.00    -0.08       0.00    -0.04
    10   1.0876      0.00     0.00       0.00    -0.23
    11   1.0876      0.00    -0.34       0.00    -0.15
    12   1.0929      0.00    -0.03       0.00    -0.06
    13   1.0929      0.00    -0.04       0.00     0.11
    14   1.0929      0.00     0.06       0.00     0.00
    15   1.1175      0.00     0.29       0.00     0.41
    16   1.1175      0.00     0.35       0.00     0.40
    17   1.1937      0.00     0.08       0.00     0.00
    18   1.1939      0.00     0.04       0.00     0.04
    19   2.0103      0.00     0.05       0.00    -0.18
    20   2.0103      0.00    -0.08       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.

14KL84    quality flag:3

Type:       CENTAURR  CENTAURR  CENTAURR

axisobj        15.972    15.971    15.972
ecceobj         0.640     0.640     0.640
incobj         12.258    12.258    12.258
qmin            5.755     5.755     5.755
qmax           26.188    26.188    26.189
amean          15.972    15.972    15.972
amin           15.972    15.972    15.972
amax           15.972    15.972    15.972
emean           0.640     0.640     0.640
emin            0.640     0.640     0.640
emax            0.640     0.640     0.640
imean          10.873    10.873    10.873
imin           10.873    10.873    10.873
imax           10.873    10.873    10.873
excite_mean     0.667     0.667     0.667
fracstop        0.000     0.000     0.000
cjmean          2.986     2.986     2.986

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        91.3      91.3      91.3
kozaiamp          0.0       0.0       0.0