Orbit Fit and Astrometric record for 15HZ196

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: 15HZ196   
# Created Wed May  8 01:17:07 2024
# Orbit generated from Bernstein formalism
# Fitting     35 observations of     35
# Arc:   2.11y
# First observation: 2015/02/17
#  Last observation: 2017/03/29
Preliminary a, adot, b, bdot, g, gdot:
  -0.000150   0.024626   0.000002  -0.000722   0.024467   0.000000
# Chi-squared of fit:     4.38 DOF:     64 RMS:  0.06
# Min/Max residuals:    -0.18    0.20
# Exact a, adot, b, bdot, g, gdot:
  1.572025E-05  2.445874E-02 -3.678444E-07 -7.182886E-04  2.451299E-02  3.646008E-04
# Covariance matrix:
  2.0301E-13 -2.6636E-15  2.0519E-16 -2.7127E-15  1.5362E-13  2.1053E-12
 -2.6636E-15  2.9115E-13  1.4207E-15 -8.4921E-15  1.6952E-13  6.4636E-12
  2.0519E-16  1.4207E-15  8.9243E-14 -6.5710E-14  9.4314E-16  4.5570E-14
 -2.7127E-15 -8.4921E-15 -6.5710E-14  9.0862E-14 -7.2249E-15 -2.7360E-13
  1.5362E-13  1.6952E-13  9.4314E-16 -7.2249E-15  2.5046E-13  5.5424E-12
  2.1053E-12  6.4636E-12  4.5570E-14 -2.7360E-13  5.5424E-12  2.0828E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
    0.745694 -154.077567    0.832678    0.007001   -0.526685  2457071.015468
# Heliocentric elements and errors
Epoch:              2457070.5000  =  2015/02/17
Mean Anomaly:          356.22966 +/-     0.693
Argument of Peri:      160.28034 +/-     0.762
Long of Asc Node:       48.61370 +/-     0.009
Inclination:             1.81983 +/-     0.001
Eccentricity:         0.04628341 +/-    0.0001
Semi-Major Axis:     43.33308009 +/-    0.0027
Time of Perihelion: 2458161.7029 +/-     200.6
Perihelion:          41.32747729 +/-    0.0036
Aphelion:            45.33868288 +/-    0.0038
Period (y)              285.2578 +/-      0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -37.52757789 +/-    0.0008
Ecliptic Y          -17.31339041 +/-    0.0004
Ecliptic Z            0.53090073 +/-    0.0000
Ecliptic XDOT         0.00115300 +/-    0.0000
Ecliptic YDOT        -0.00248076 +/-    0.0000
Ecliptic ZDOT        -0.00007960 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   41.33224462 +/-    0.0007
Geocenter to KBO     40.79468886 +/-    0.0008
# Hcoef:  7.01

The following table shows the complete astrometric record for 15HZ196. 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 (15HZ196) followed by the observatory code and reference code for the source of the astrometry.

2015 02  17.51469  13 37 14.153  -09 19 09.14  23.0r 15HZ196   568  C~2nvf      
2015 02  17.55579  13 37 14.064  -09 19 08.62  23.1r 15HZ196   568  C~2nvf      
2015 02  20.48657  13 37 07.760  -09 18 30.57  23.2r 15HZ196   568  C~2nvf      
2015 03  18.49249  13 35 44.810  -09 10 22.05  23.3r 15HZ196   568  C~2nvf      
2015 03  18.53407  13 35 44.636  -09 10 21.07  23.3r 15HZ196   568  C~2nvf      
2015 04  11.47256  13 33 59.902  -09 00 16.39  23.0r 15HZ196   568  C~2nvf      
2015 04  12.37938  13 33 55.714  -08 59 52.36  22.9r 15HZ196   568  C~2nvf      
2015 04  12.42509  13 33 55.493  -08 59 51.05  23.0r 15HZ196   568  C~2nvf      
2015 04  12.46730  13 33 55.296  -08 59 49.96  22.8r 15HZ196   568  C~2nvf      
2015 04  19.28870  13 33 23.67   -08 56 48.9         15HZ196   W84  C#00TE      
2015 04  21.28968  13 33 14.41   -08 55 56.1   23.4V 15HZ196   W84  C#00TE      
2015 04  22.28936  13 33 09.80   -08 55 29.8         15HZ196   W84  C#00TE      
2015 05  16.28656  13 31 26.330  -08 45 46.40  23.1r 15HZ196   568  C~2nvf      
2015 05  17.24686  13 31 22.633  -08 45 25.74  23.3r 15HZ196   568  C~2nvf      
2015 05  25.38864  13 30 53.226  -08 42 43.07  22.9r 15HZ196   568  C~2nvf      
2015 05  25.44647  13 30 53.029  -08 42 42.02  23.0r 15HZ196   568  C~2nvf      
2015 06  22.29486  13 29 45.999  -08 36 47.31  23.1r 15HZ196   568  C~2nvf      
2015 07  12.28879  13 29 36.709  -08 36 23.66  23.2r 15HZ196   568  C~2nvf      
2015 07  15.27909  13 29 38.356  -08 36 38.12  23.2r 15HZ196   568  C~2nvf      
2015 07  19.27863  13 29 41.802  -08 37 04.50  23.4r 15HZ196   568  C~2nvf      
2016 02  04.61430  13 42 46.796  -09 53 38.42  23.5w 15HZ196   568  C~2nvf      
2016 02  11.59752  13 42 39.357  -09 52 51.75  23.4w 15HZ196   568  C~2nvf      
2016 04  03.47768  13 39 51.282  -09 36 39.94  23.2w 15HZ196   568  C~2nvf      
2016 04  09.45883  13 39 23.961  -09 34 05.02  23.2w 15HZ196   568  C~2nvf      
2016 05  02.35991  13 37 38.698  -09 24 12.82  23.1w 15HZ196   568  C~2nvf      
2016 05  07.36327  13 37 16.865  -09 22 11.20  23.4w 15HZ196   568  C~2nvf      
2016 05  29.32744  13 35 53.701  -09 14 34.10  23.4w 15HZ196   568  C~2nvf      
2016 06  04.38987  13 35 35.587  -09 12 56.93  23.4w 15HZ196   568  C~2nvf      
2016 06  27.32010  13 34 52.035  -09 09 16.53  23.9w 15HZ196   568  C~2nvf      
2016 06  27.32513  13 34 52.029  -09 09 16.57  23.4w 15HZ196   568  C~2nvf      
2016 07  07.31590  13 34 46.771  -09 09 00.97  23.4w 15HZ196   568  C~2nvf      
2017 02  27.64150  13 47 21.521  -10 21 55.45        15HZ196   568  C~2nvf      
2017 02  27.66186  13 47 21.478  -10 21 55.03        15HZ196   568  C~2nvf      
2017 03  29.48748  13 45 33.856  -10 11 45.57  23.6w 15HZ196   568  C~2nvf      
2017 03  29.50900  13 45 33.765  -10 11 44.94  23.4w 15HZ196   568  C~2nvf      

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     -1.42    -0.03       0.01    -0.02
     3   0.0081   -102.18     0.01       1.63    -0.02
     4   0.0793  -1423.86     0.07      10.94     0.00
     5   0.0795  -1426.62    -0.01      10.92    -0.01
     6   0.1450  -3091.80    -0.09       9.31    -0.02
     7   0.1475  -3158.35    -0.07       9.06    -0.04
     8   0.1476  -3161.88    -0.18       9.09     0.02
     9   0.1477  -3164.99    -0.14       9.04     0.01
    10   0.1664  -3667.48     0.17       6.65     0.11
    11   0.1719  -3814.54     0.06       5.71     0.12
    12   0.1746  -3887.77     0.03       5.25     0.16
    13   0.2403  -5529.35     0.06     -12.61    -0.06
    14   0.2429  -5587.96     0.03     -13.46    -0.01
    15   0.2652  -6053.60    -0.03     -21.87    -0.02
    16   0.2654  -6056.71     0.02     -21.96    -0.03
    17   0.3416  -7112.59    -0.02     -56.73     0.01
    18   0.3964  -7249.59    -0.03     -85.36     0.04
    19   0.4046  -7221.52     0.08     -89.84    -0.07
    20   0.4155  -7164.23     0.02     -95.60     0.00
    21   0.9640   5336.04     0.02    -155.62    -0.03
    22   0.9831   5216.61     0.01    -151.50    -0.02
    23   1.1252   2547.64     0.06    -138.85    -0.03
    24   1.1415   2114.82     0.01    -140.22    -0.04
    25   1.2042    448.63     0.00    -151.38    -0.00
    26   1.2179    103.41     0.06    -155.12    -0.02
    27   1.2781  -1209.60     0.02    -176.02    -0.02
    28   1.2947  -1494.78    -0.04    -183.00    -0.02
    29   1.3574  -2175.73    -0.06    -212.36    -0.01
    30   1.3575  -2175.80    -0.05    -212.43    -0.07
    31   1.3848  -2254.01    -0.01    -226.25    -0.09
    32   2.0291   9737.25    -0.08    -292.10     0.03
    33   2.0292   9736.51     0.06    -291.93     0.20
    34   2.1108   8032.03    -0.01    -288.09    -0.07
    35   2.1109   8030.54     0.01    -287.98     0.05

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.

15HZ196    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        42.924    42.932    42.915
ecceobj         0.037     0.037     0.037
incobj          1.825     1.825     1.825
qmin           40.684    40.667    40.656
qmax           45.912    45.938    45.927
amean          43.206    43.215    43.198
amin           42.872    42.877    42.863
amax           43.550    43.558    43.536
emean           0.036     0.036     0.036
emin            0.018     0.017     0.017
emax            0.055     0.055     0.055
imean           1.254     1.254     1.254
imin            0.224     0.228     0.219
imax            1.976     1.976     1.977
excite_mean     0.043     0.043     0.043
fracstop        1.000     1.000     1.000
cjmean          3.090     3.090     3.090

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       164.4     164.0     164.4
kozaiamp        179.9     180.0     180.0