Orbit Fit and Astrometric record for 15KH174

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: 15KH174   
# Created Fri Nov 22 02:10:23 2024
# Orbit generated from Bernstein formalism
# Fitting     36 observations of     36
# Arc:   3.24y
# First observation: 2014/05/31
#  Last observation: 2017/08/27
Preliminary a, adot, b, bdot, g, gdot:
  -0.000113   0.033214  -0.000012   0.005333   0.028657   0.000000
# Chi-squared of fit:     3.05 DOF:     66 RMS:  0.05
# Min/Max residuals:    -0.11    0.18
# Exact a, adot, b, bdot, g, gdot:
  1.823677E-05  3.282425E-02  2.062190E-06  5.271403E-03  2.846060E-02 -9.457211E-03
# Covariance matrix:
  2.2543E-13 -2.9238E-13  1.6893E-14 -3.6433E-14 -7.5595E-14 -2.4160E-12
 -2.9238E-13  5.7669E-13 -3.9680E-14  8.4946E-14  1.1351E-13  5.7236E-12
  1.6893E-14 -3.9680E-14  1.2648E-13 -7.4449E-14 -7.6758E-15 -4.3756E-13
 -3.6433E-14  8.4946E-14 -7.4449E-14  6.9393E-14  1.7782E-14  9.3425E-13
 -7.5595E-14  1.1351E-13 -7.6758E-15  1.7782E-14  1.5819E-13  1.0041E-12
 -2.4160E-12  5.7236E-12 -4.3756E-13  9.3425E-13  1.0041E-12  6.3302E-11
#      lat0       lon0       xBary       yBary       zBary        JD0
    5.191614 -124.928231   -0.258617    0.088862   -0.977454  2456808.928768
# Heliocentric elements and errors
Epoch:              2456800.5000  =  2014/05/23
Mean Anomaly:          338.50258 +/-     0.010
Argument of Peri:       83.32836 +/-     0.028
Long of Asc Node:      206.49251 +/-     0.001
Inclination:            10.33562 +/-     0.000
Eccentricity:         0.42659876 +/-    0.0002
Semi-Major Axis:     55.23472016 +/-    0.0124
Time of Perihelion: 2465754.1560 +/-       2.7
Perihelion:          31.67165715 +/-    0.0142
Aphelion:            78.79778317 +/-    0.0216
Period (y)              410.5126 +/-      0.14
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -20.38597727 +/-    0.0003
Ecliptic Y          -29.64031473 +/-    0.0004
Ecliptic Z            3.17950560 +/-    0.0000
Ecliptic XDOT         0.00312861 +/-    0.0000
Ecliptic YDOT        -0.00103110 +/-    0.0000
Ecliptic ZDOT         0.00042282 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   36.11434039 +/-    0.0004
Geocenter to KBO     35.13629145 +/-    0.0005
# Hcoef:  7.65

The following table shows the complete astrometric record for 15KH174. 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 (15KH174) followed by the observatory code and reference code for the source of the astrometry.

2014 05  31.42799  15 36 02.575  -13 59 27.20  20.7r 15KH174   568  C~2lVJ      
2014 06  01.31617  15 35 57.972  -13 59 10.50  23.3r 15KH174   568  C~2lVJ      
2014 06  01.35941  15 35 57.743  -13 59 09.67  23.1r 15KH174   568  C~2lVJ      
2014 06  01.40234  15 35 57.515  -13 59 08.95  23.0r 15KH174   568  C~2lVJ      
2014 06  22.31374  15 34 18.544  -13 53 37.42  23.2r 15KH174   568  C~2lVJ      
2014 06  22.35659  15 34 18.364  -13 53 36.92  23.4r 15KH174   568  C~2lVJ      
2015 02  23.61954  15 49 31.871  -14 39 11.60  23.5r 15KH174   568  C~2lVJ      
2015 03  19.57896  15 49 18.382  -14 33 41.52  23.4r 15KH174   568  C~2lVJ      
2015 03  21.63764  15 49 14.282  -14 33 05.25  23.3r 15KH174   568  C~2lVJ      
2015 04  18.51897  15 47 40.654  -14 23 30.58  23.4r 15KH174   568  C~2lVJ      
2015 05  17.39179  15 45 14.131  -14 12 43.66  23.2r 15KH174   568  C~2lVJ      
2015 05  17.43344  15 45 13.888  -14 12 42.77  23.1r 15KH174   568  C~2lVJ      
2015 05  17.48044  15 45 13.626  -14 12 41.75  23.3r 15KH174   568  C~2lVJ      
2015 05  17.48543  15 45 13.606  -14 12 41.71  23.2r 15KH174   568  C~2lVJ      
2015 05  17.51054  15 45 13.465  -14 12 41.08  23.1r 15KH174   568  C~2lVJ      
2015 05  24.37741  15 44 36.123  -14 10 18.25  23.2r 15KH174   568  C~2lVJ      
2015 05  24.42349  15 44 35.873  -14 10 17.36  23.3r 15KH174   568  C~2lVJ      
2015 05  24.46441  15 44 35.639  -14 10 16.46  23.2r 15KH174   568  C~2lVJ      
2015 05  26.45236  15 44 24.880  -14 09 36.70  23.1r 15KH174   568  C~2lVJ      
2015 06  18.35156  15 42 28.653  -14 03 08.35  22.9r 15KH174   568  C~2lVJ      
2015 06  18.39254  15 42 28.467  -14 03 07.81  23.2r 15KH174   568  C~2lVJ      
2015 06  21.36717  15 42 15.085  -14 02 28.71  23.2r 15KH174   568  C~2lVJ      
2015 07  10.42339  15 41 04.064  -13 59 34.08  23.2r 15KH174   568  C~2lVJ      
2015 07  18.32575  15 40 43.499  -13 59 02.93  23.1r 15KH174   568  C~2lVJ      
2015 07  18.34810  15 40 43.454  -13 59 03.05  23.3r 15KH174   568  C~2lVJ      
2016 04  03.58309  15 56 39.348  -14 35 49.30  23.5w 15KH174   568  C~2lVJ      
2016 04  08.63261  15 56 21.855  -14 34 04.62  23.3w 15KH174   568  C~2lVJ      
2016 04  09.57657  15 56 18.358  -14 33 44.55  23.5w 15KH174   568  C~2lVJ      
2016 04  29.52576  15 54 49.830  -14 26 27.17  23.3w 15KH174   568  C~2lVJ      
2016 05  04.49833  15 54 24.411  -14 24 37.12  23.3w 15KH174   568  C~2lVJ      
2016 05  30.44177  15 52 03.712  -14 15 44.62  23.4w 15KH174   568  C~2lVJ      
2016 07  04.32652  15 49 20.168  -14 08 00.88  23.4w 15KH174   568  C~2lVJ      
2016 07  05.39888  15 49 16.335  -14 07 53.22  23.4w 15KH174   568  C~2lVJ      
2017 07  17.26622  15 56 47.613  -14 14 00.09  23.4w 15KH174   568  C~2lVJ      
2017 08  25.25930  15 56 21.797  -14 17 20.84  23.4w 15KH174   568  C~2lVJ      
2017 08  27.25133  15 56 25.017  -14 17 45.91  23.6w 15KH174   568  C~2lVJ      

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     0.18
     2   0.0024    -69.05    -0.01       0.51     0.01
     3   0.0026    -72.48    -0.03       0.53     0.03
     4   0.0027    -75.88    -0.03       0.45    -0.06
     5   0.0599  -1554.30    -0.01     -16.88     0.01
     6   0.0600  -1556.96     0.04     -17.01    -0.01
     7   0.7343  12009.49     0.01     356.65     0.01
     8   0.7999  11744.83    -0.02     635.83     0.03
     9   0.8055  11678.55    -0.01     658.09    -0.06
    10   0.8818  10221.03    -0.09     917.14     0.00
    11   0.9609   7996.16     0.09    1070.71    -0.01
    12   0.9610   7992.52    -0.09    1070.78    -0.05
    13   0.9611   7988.57    -0.11    1070.92    -0.04
    14   0.9611   7988.28     0.01    1070.89    -0.08
    15   0.9612   7986.13    -0.04    1071.04     0.00
    16   0.9800   7424.09     0.05    1087.68    -0.01
    17   0.9801   7420.34     0.12    1087.72    -0.03
    18   0.9803   7416.81    -0.01    1087.83     0.01
    19   0.9857   7255.19    -0.02    1091.19     0.02
    20   1.0484   5518.65    -0.02    1085.29    -0.01
    21   1.0485   5515.89     0.07    1085.20    -0.01
    22   1.0566   5317.23    -0.02    1078.82     0.01
    23   1.1088   4270.53    -0.03    1012.09     0.01
    24   1.1305   3971.93    -0.01     973.62     0.10
    25   1.1305   3971.32     0.12     973.36    -0.04
    26   1.8430  18055.24     0.06    1904.65    -0.04
    27   1.8568  17782.78    -0.02    1952.85    -0.10
    28   1.8594  17728.50     0.02    1961.63     0.03
    29   1.9140  16369.80     0.07    2113.37    -0.01
    30   1.9276  15983.13     0.01    2141.26     0.01
    31   1.9987  13860.40     0.01    2217.15    -0.02
    32   2.0942  11429.10    -0.04    2146.54     0.00
    33   2.0971  11372.85    -0.02    2141.66    -0.07
    34   3.1289  17893.00    -0.04    3214.43     0.10
    35   3.2357  17566.57    -0.03    2936.93     0.02
    36   3.2411  17618.02     0.01    2922.41     0.03

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.

15KH174    quality flag:3

Type:         5:2EEE    5:2EEE    5:2EEE

axisobj        54.919    54.947    54.892
ecceobj         0.426     0.427     0.426
incobj         10.370    10.370    10.370
qmin           31.000    30.919    30.961
qmax           81.202    81.341    81.345
amean          55.462    55.462    55.462
amin           54.769    54.731    54.770
amax           56.378    56.424    56.415
emean           0.430     0.431     0.431
emin            0.420     0.420     0.420
emax            0.441     0.443     0.442
imean          10.683    10.635    10.634
imin           10.500    10.389    10.400
imax           10.902    10.891    10.921
excite_mean     0.468     0.469     0.468
fracstop        1.000     1.000     1.000
cjmean          2.951     2.950     2.951

libcent 0       180.3     180.1     181.0
libamp  0        72.9      78.0      78.0
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       159.0     167.7     168.7
kozaiamp         87.3      97.4      97.3