Orbit Fit and Astrometric record for 15KK166

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: 15KK166   
# Created Fri Jan 24 02:10:49 2025
# Orbit generated from Bernstein formalism
# Fitting     21 observations of     21
# Arc:  56.91d
# First observation: 2015/05/17
#  Last observation: 2015/07/13
Preliminary a, adot, b, bdot, g, gdot:
  -0.000003   0.030939  -0.000009   0.002197   0.026782   0.000000
# Chi-squared of fit:     5.43 DOF:     36 RMS:  0.09
# Min/Max residuals:    -0.18    0.26
# Exact a, adot, b, bdot, g, gdot:
  1.629318E-05  2.668430E-02  6.775288E-07  1.083516E-03  2.612752E-02  2.488886E-04
# Covariance matrix:
  3.9054E-13  3.2063E-11 -3.8538E-14  7.9476E-12  8.9174E-12  3.1944E-10
  3.2063E-11  4.5709E-08 -8.9375E-11  1.1892E-08  7.4464E-09 -1.0075E-06
 -3.8538E-14 -8.9375E-11  3.2301E-13 -2.4372E-11 -1.4147E-11  2.0946E-09
  7.9476E-12  1.1892E-08 -2.4372E-11  3.1111E-09  1.9272E-09 -2.6534E-07
  8.9174E-12  7.4464E-09 -1.4147E-11  1.9272E-09  1.2695E-09 -1.4748E-07
  3.1944E-10 -1.0075E-06  2.0946E-09 -2.6534E-07 -1.4748E-07  2.7183E-05
#      lat0       lon0       xBary       yBary       zBary        JD0
   14.592768 -139.900227   -0.278915    0.244534   -0.938897  2457159.910491
# Heliocentric elements and errors
Epoch:              2457150.5000  =  2015/05/08
Mean Anomaly:           23.35241 +/-   223.181
Argument of Peri:       55.91823 +/-   245.896
Long of Asc Node:      139.37493 +/-     0.181
Inclination:            14.39915 +/-     0.006
Eccentricity:         0.04407155 +/-    0.0742
Semi-Major Axis:     40.85626143 +/-    0.3099
Time of Perihelion: 2450962.9947 +/-   59134.5
Perihelion:          39.05566264 +/-    3.0452
Aphelion:            42.65686022 +/-    3.0480
Period (y)              261.1537 +/-      2.97
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -28.89752427 +/-    0.0386
Ecliptic Y          -24.69635856 +/-    0.0325
Ecliptic Z            9.64306356 +/-    0.0132
Ecliptic XDOT         0.00180083 +/-    0.0004
Ecliptic YDOT        -0.00214283 +/-    0.0003
Ecliptic ZDOT         0.00011652 +/-    0.0001
# Distances at JD0 (AU)
Heliocenter to KBO   39.21690592 +/-    0.0352
Geocenter to KBO     38.27382162 +/-    0.0522
# Hcoef:  7.88

The following table shows the complete astrometric record for 15KK166. 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 (15KK166) followed by the observatory code and reference code for the source of the astrometry.

2015 05  17.409713 14 48 57.248  -00 57 44.20  24.3g 15KK166   568  C~2TuP      
2015 05  17.473611 14 48 56.935  -00 57 43.16  24.1g 15KK166   568  C~2TuP      
2015 05  17.475730 14 48 56.930  -00 57 43.08  24.0g 15KK166   568  C~2TuP      
2015 05  21.378768 14 48 38.486  -00 56 40.06  23.4i 15KK166   568  C~2TuP      
2015 05  21.384867 14 48 38.458  -00 56 39.98  23.3i 15KK166   568  C~2TuP      
2015 05  21.387551 14 48 38.442  -00 56 39.91  23.3i 15KK166   568  C~2TuP      
2015 05  21.395625 14 48 38.405  -00 56 39.83  23.5i 15KK166   568  C~2TuP      
2015 05  21.403709 14 48 38.367  -00 56 39.68  23.3i 15KK166   568  C~2TuP      
2015 05  26.36079  14 48 15.56   -00 55 31.1   23.1y 15KK166   T09  C~8SVr      
2015 05  26.42612  14 48 15.25   -00 55 30.5   23.7y 15KK166   T09  C~8SVr      
2015 05  26.43645  14 48 15.20   -00 55 30.1   23.2y 15KK166   T09  C~8SVr      
2015 05  26.46546  14 48 15.08   -00 55 29.8   24.4y 15KK166   T09  C~8SVr      
2015 07  12.27784  14 45 46.71   -00 56 17.2   23.8z 15KK166   T09  C~8SVr      
2015 07  12.29403  14 45 46.68   -00 56 17.5   23.7z 15KK166   T09  C~8SVr      
2015 07  12.29672  14 45 46.69   -00 56 17.4   24.1z 15KK166   T09  C~8SVr      
2015 07  12.31304  14 45 46.67   -00 56 17.9   23.4z 15KK166   T09  C~8SVr      
2015 07  12.33461  14 45 46.62   -00 56 17.9   23.4z 15KK166   T09  C~8SVr      
2015 07  12.35079  14 45 46.59   -00 56 18.4   23.6z 15KK166   T09  C~8SVr      
2015 07  13.28875  14 45 45.32   -00 56 32.2   24.3r 15KK166   T09  C~8SVr      
2015 07  13.30229  14 45 45.31   -00 56 32.3   24.3r 15KK166   T09  C~8SVr      
2015 07  13.31727  14 45 45.30   -00 56 32.5   24.3r 15KK166   T09  C~8SVr      

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    -0.03       0.00    -0.00
     2   0.0002     -4.79    -0.05      -0.44    -0.07
     3   0.0002     -4.88     0.01      -0.38    -0.00
     4   0.0109   -287.56     0.03     -24.54     0.02
     5   0.0109   -287.99     0.05     -24.59     0.01
     6   0.0109   -288.24    -0.00     -24.59     0.03
     7   0.0109   -288.79     0.03     -24.69    -0.01
     8   0.0109   -289.38     0.03     -24.72     0.02
     9   0.0245   -636.09     0.03     -63.50     0.06
    10   0.0247   -640.70    -0.03     -64.34    -0.18
    11   0.0247   -641.53    -0.15     -64.19     0.06
    12   0.0248   -643.34     0.06     -64.45     0.06
    13   0.1530  -2748.70     0.03    -787.12     0.01
    14   0.1530  -2749.04    -0.04    -787.54    -0.08
    15   0.1530  -2748.93     0.12    -787.40     0.12
    16   0.1531  -2749.06     0.26    -787.97    -0.12
    17   0.1531  -2749.78    -0.09    -788.20     0.10
    18   0.1532  -2750.05    -0.10    -788.81    -0.18
    19   0.1557  -2764.00    -0.17    -807.76    -0.07
    20   0.1558  -2764.11    -0.07    -807.90     0.07
    21   0.1558  -2764.19     0.07    -808.14     0.14

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.

15KK166    quality flag:1

Type:      CLASSICAL  CENTAURR CLASSICAL

axisobj        40.479    57.194    39.946
ecceobj         0.035     0.530     0.024
incobj         14.413    14.424    14.392
qmin           38.309    26.597    37.855
qmax           43.377    89.945    42.739
amean          40.758    57.137    40.217
amin           40.449    54.704    39.920
amax           41.079    58.673    40.521
emean           0.036     0.522     0.027
emin            0.018     0.492     0.003
emax            0.056     0.537     0.055
imean          13.388    13.773    13.391
imin           12.446    12.881    12.184
imax           14.672    15.425    15.049
excite_mean     0.234     0.574     0.233
fracstop        1.000     0.059     1.000
cjmean          3.002     2.815     2.997

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       178.8     189.2     178.5
kozaiamp        180.0      21.3     180.0