Orbit Fit and Astrometric record for 15KW175

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: 15KW175   
# Created Sun Nov 24 02:10:21 2024
# Orbit generated from Bernstein formalism
# Fitting     33 observations of     35
# Arc:   3.24y
# First observation: 2014/05/29
#  Last observation: 2017/08/26
Preliminary a, adot, b, bdot, g, gdot:
   0.000249   0.027415  -0.000021  -0.001297   0.025781   0.000000
# Chi-squared of fit:    11.32 DOF:     60 RMS:  0.10
# Min/Max residuals:    -0.25    0.28
# Exact a, adot, b, bdot, g, gdot:
  1.618915E-05  2.787252E-02 -2.427514E-07 -1.332697E-03  2.600865E-02 -1.707297E-04
# Covariance matrix:
  2.6357E-13 -3.2924E-13 -1.1561E-14  1.8378E-14 -9.1690E-14 -3.1518E-12
 -3.2924E-13  6.3173E-13  2.6255E-14 -4.2730E-14  1.6393E-13  7.1692E-12
 -1.1561E-14  2.6255E-14  1.4731E-13 -7.3401E-14  6.8852E-15  3.2465E-13
  1.8378E-14 -4.2730E-14 -7.3401E-14  5.3809E-14 -8.5295E-15 -5.3236E-13
 -9.1690E-14  1.6393E-13  6.8852E-15 -8.5295E-15  1.6232E-13  1.8496E-12
 -3.1518E-12  7.1692E-12  3.2465E-13 -5.3236E-13  1.8496E-12  8.8695E-11
#      lat0       lon0       xBary       yBary       zBary        JD0
    5.860882 -127.053544   -0.261313    0.100161   -0.975228  2456806.882768
# Heliocentric elements and errors
Epoch:              2456800.5000  =  2014/05/23
Mean Anomaly:            0.83835 +/-     0.110
Argument of Peri:      114.74416 +/-     0.150
Long of Asc Node:      117.27244 +/-     0.004
Inclination:             6.35679 +/-     0.000
Eccentricity:         0.14805583 +/-    0.0001
Semi-Major Axis:     46.27481266 +/-    0.0034
Time of Perihelion: 2456532.7453 +/-      35.1
Perihelion:          39.42355690 +/-    0.0041
Aphelion:            53.12606841 +/-    0.0049
Period (y)              314.7931 +/-      0.04
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -23.43012761 +/-    0.0004
Ecliptic Y          -31.46290787 +/-    0.0005
Ecliptic Z            3.92618142 +/-    0.0001
Ecliptic XDOT         0.00233847 +/-    0.0000
Ecliptic YDOT        -0.00176875 +/-    0.0000
Ecliptic ZDOT        -0.00014127 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   39.42461607 +/-    0.0004
Geocenter to KBO     38.44875019 +/-    0.0006
# Hcoef:  8.58

The following table shows the complete astrometric record for 15KW175. 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 (15KW175) followed by the observatory code and reference code for the source of the astrometry.

2014 05  29.38199  15 28 15.601  -12 49 58.46  24.0r 15KW175   568  C~2nvi      
2014 05  29.42085  15 28 15.388  -12 49 57.44  25.2r 15KW175   568  C~2nvi      
2014 05  31.40597  15 28 05.808  -12 49 28.75  24.4r 15KW175   568  C~2nvi      
2014 06  22.30598  15 26 30.347  -12 45 23.70  24.7r 15KW175   568  C~2nvi      
2014 06  22.34880  15 26 30.155  -12 45 23.36  24.6r 15KW175   568  C~2nvi      
2014 07  19.32186  15 25 14.577  -12 44 14.89  24.5r 15KW175   568  C~2nvi      
2015 02  20.65667  15 39 50.061  -13 42 51.02  25.3r 15KW175   568  C~2nvi      
2015 03  19.57074  15 39 30.100  -13 38 08.55  23.9r 15KW175   568  C~2nvi      
2015 04  12.52910  15 38 16.728  -13 31 32.66  24.4r 15KW175   568  C~2nvi      
2015 05  17.38343  15 35 33.940  -13 20 56.21  24.0r 15KW175   568  C~2nvi      
2015 05  17.42514  15 35 33.712  -13 20 55.41  24.3r 15KW175   568  C~2nvi      
2015 05  17.46733  15 35 33.522  -13 20 54.79  24.6r 15KW175   568  C~2nvi      
2015 05  24.36911  15 34 58.792  -13 19 01.87  24.1r 15KW175   568  C~2nvi      
2015 05  24.41533  15 34 58.551  -13 19 01.02  24.5r 15KW175   568  C~2nvi      
2015 05  24.45620  15 34 58.344  -13 19 00.27  24.4r 15KW175   568  C~2nvi      
2015 05  26.44379  15 34 48.426  -13 18 29.69  24.2r 15KW175   568  C~2nvi      
2015 06  18.34328  15 33 02.382  -13 13 44.76  24.5r 15KW175   568  C~2nvi      
2015 06  18.38434  15 33 02.186  -13 13 44.61  24.7r 15KW175   568  C~2nvi      
2015 06  21.35896  15 32 50.116  -13 13 19.03  24.8r 15KW175   568  C~2nvi      
2015 07  17.34619  15 31 30.435  -13 11 48.62  24.1r 15KW175   568  C~2nvi      
2015 07  18.31678  15 31 28.507  -13 11 50.28  24.7r 15KW175   568  C~2nvi      
2016 02  06.62508  15 45 39.150  -14 09 37.03  25.1w 15KW175   568  C~2nvi      
2016 02  12.61062  15 45 51.047  -14 09 27.86  25.0w 15KW175   568  C~2nvi      
2016 03  15.61859  15 45 51.095  -14 05 12.69  24.6w 15KW175   568  C~2nvi      
2016 04  03.55474  15 45 04.108  -14 00 33.68  24.6w 15KW175   568  C~2nvi      
2016 04  08.60428  15 44 46.637  -13 59 09.00  24.6w 15KW175   568  C~2nvi      
2016 04  29.47374  15 43 18.043  -13 52 58.91  23.9w 15KW175   568  C~2nvj      
2016 05  04.40882  15 42 54.301  -13 51 30.84  24.7w 15KW175   568  C~2nvj      
2016 07  04.29413  15 38 17.376  -13 39 11.81  25.0w 15KW175   568  C~2nvj      
2016 07  05.36242  15 38 14.033  -13 39 08.22  25.1w 15KW175   568  C~2nvj      
2017 05  21.53337  15 47 50.590  -14 13 16.82  24.4w 15KW175   568  C~2nvj      
2017 07  28.31194  15 43 39.346  -14 06 00.77        15KW175   568  C~2nvj      
2017 08  19.27024  15 43 34.815  -14 09 11.89  24.9w 15KW175   568  C~2nvj      
2017 08  25.27821  15 43 41.945  -14 10 32.88  25.1w 15KW175   568  C~2nvj      
2017 08  26.25868  15 43 43.471  -14 10 47.19  25.2w 15KW175   568  C~2nvj      

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     0.16       0.00    -0.12
     2   0.0001     -3.27    -0.24       0.22     0.24
     3   0.0055   -146.14     0.03      -6.42    -0.06
     4   0.0655  -1559.84 (   0.55)   -113.47 (   0.11)
     5   0.0656  -1562.65     0.19    -113.84     0.03
     6   0.1395  -2650.92    -0.03    -321.81     0.03
     7   0.7318  10613.10    -0.02    -644.27     0.00
     8   0.8054  10263.08 (   0.49)   -437.70 (   0.05)
     9   0.8710   9127.61     0.07    -304.73    -0.06
    10   0.9665   6665.80    -0.03    -250.41    -0.09
    11   0.9666   6662.38    -0.25    -250.43    -0.05
    12   0.9667   6659.53     0.16    -250.49    -0.05
    13   0.9856   6139.83     0.14    -262.05    -0.03
    14   0.9857   6136.21     0.03    -262.07     0.07
    15   0.9858   6133.09     0.02    -262.06     0.18
    16   0.9913   5985.08    -0.02    -267.04    -0.07
    17   1.0540   4412.78     0.13    -362.67     0.28
    18   1.0541   4409.97    -0.13    -363.22    -0.01
    19   1.0622   4232.68     0.01    -380.93    -0.06
    20   1.1334   3081.45    -0.16    -574.92    -0.00
    21   1.1360   3054.53    -0.15    -583.37    -0.10
    22   1.6927  15951.46    -0.13   -1031.07    -0.15
    23   1.7090  16118.82     0.05    -982.49    -0.10
    24   1.7967  16060.82     0.00    -733.14    -0.05
    25   1.8485  15327.14    -0.06    -617.59     0.01
    26   1.8623  15058.76     0.06    -593.42     0.05
    27   1.9195  13711.86     0.06    -530.09    -0.02
    28   1.9330  13353.58     0.03    -524.34     0.06
    29   2.0997   9245.47    -0.01    -749.12    -0.09
    30   2.1026   9197.18     0.16    -757.14    -0.02
    31   2.9792  17875.62    -0.11    -809.85     0.05
    32   3.1648  14196.36     0.08   -1220.91    -0.01
    33   3.2249  14176.26     0.04   -1422.56     0.11
    34   3.2413  14296.42    -0.13   -1477.61    -0.01
    35   3.2440  14321.44     0.07   -1486.45     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.

15KW175    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        45.960    45.971    45.948
ecceobj         0.143     0.143     0.142
incobj          6.353     6.353     6.353
qmin           39.002    38.972    38.976
qmax           54.020    54.063    54.036
amean          46.350    46.362    46.336
amin           45.949    45.970    45.931
amax           46.795    46.805    46.776
emean           0.142     0.142     0.142
emin            0.130     0.129     0.128
emax            0.156     0.156     0.156
imean           4.765     4.765     4.766
imin            4.235     4.235     4.234
imax            5.309     5.310     5.312
excite_mean     0.165     0.165     0.164
fracstop        1.000     1.000     1.000
cjmean          3.097     3.097     3.097

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       182.1     182.1     181.9
kozaiamp        180.0     179.9     180.0