Orbit Fit and Astrometric record for 15VK173

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: 15VK173   
# Created Tue Apr  1 01:10:43 2025
# Orbit generated from Bernstein formalism
# Fitting     35 observations of     36
# Arc:   3.06y
# First observation: 2014/11/23
#  Last observation: 2017/12/16
Preliminary a, adot, b, bdot, g, gdot:
   0.000073   0.020893  -0.000001   0.004214   0.022888   0.000000
# Chi-squared of fit:     6.59 DOF:     64 RMS:  0.08
# Min/Max residuals:    -0.33    0.25
# Exact a, adot, b, bdot, g, gdot:
  1.465614E-05  2.108801E-02  2.930384E-06  4.250179E-03  2.301691E-02  1.103673E-03
# Covariance matrix:
  7.6913E-13 -8.5227E-13  9.8824E-14 -1.4147E-13 -3.9521E-13 -9.6770E-12
 -8.5227E-13  1.0671E-12 -1.3336E-13  1.9122E-13  5.1403E-13  1.3079E-11
  9.8824E-14 -1.3336E-13  2.4384E-13 -1.4756E-13 -6.9722E-14 -1.7684E-12
 -1.4147E-13  1.9122E-13 -1.4756E-13  1.1794E-13  9.8508E-14  2.5367E-12
 -3.9521E-13  5.1403E-13 -6.9722E-14  9.8508E-14  3.6448E-13  6.7416E-12
 -9.6770E-12  1.3079E-11 -1.7684E-12  2.5367E-12  6.7416E-12  1.7350E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
   -2.613499   47.525020   -0.223918   -0.043716   -0.961290  2456984.885458
# Heliocentric elements and errors
Epoch:              2456980.5000  =  2014/11/19
Mean Anomaly:          102.72994 +/-     0.232
Argument of Peri:      238.37632 +/-     0.224
Long of Asc Node:       60.28797 +/-     0.001
Inclination:            11.68455 +/-     0.001
Eccentricity:         0.05601866 +/-    0.0006
Semi-Major Axis:     43.73869252 +/-    0.0037
Time of Perihelion: 2426830.1985 +/-      68.0
Perihelion:          41.28850970 +/-    0.0248
Aphelion:            46.18887534 +/-    0.0248
Period (y)              289.2723 +/-      0.04
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           29.78889965 +/-    0.0007
Ecliptic Y           32.87391787 +/-    0.0009
Ecliptic Z           -1.98098347 +/-    0.0001
Ecliptic XDOT        -0.00175024 +/-    0.0000
Ecliptic YDOT         0.00180258 +/-    0.0000
Ecliptic ZDOT         0.00049915 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   44.40717638 +/-    0.0008
Geocenter to KBO     43.44632299 +/-    0.0011
# Hcoef:  7.88

The following table shows the complete astrometric record for 15VK173. 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 (15VK173) followed by the observatory code and reference code for the source of the astrometry.

2014 11  23.38468  03 03 16.677  +14 33 05.07  24.7r 15VK173   568  C~2nwH      
2015 09  06.62757  03 12 38.276  +15 25 11.69  24.8w 15VK173   568  C~2nwH      
2015 09  12.51723  03 12 28.534  +15 24 29.37  24.6w 15VK173   568  C~2nwH      
2015 10  07.45292  03 11 17.967  +15 19 45.32  24.5w 15VK173   568  C~2nwH      
2015 10  08.45753  03 11 14.252  +15 19 31.02  24.5w 15VK173   568  C~2nwH      
2015 10  08.51654  03 11 14.037  +15 19 30.13  24.9w 15VK173   568  C~2nwH      
2015 11  07.36426  03 09 04.624  +15 11 28.33  24.2r 15VK173   568  C~2nwH      
2015 11  07.40638  03 09 04.420  +15 11 27.65  24.4r 15VK173   568  C~2nwH      
2015 11  07.44859  03 09 04.217  +15 11 26.95  24.3r 15VK173   568  C~2nwH      
2015 11  10.53471  03 08 49.605  +15 10 34.98  24.4w 15VK173   568  C~2nwH      
2015 11  17.38127  03 08 17.202  +15 08 41.26  24.6w 15VK173   568  C~2nwH      
2015 11  17.42797  03 08 16.973  +15 08 40.52  24.5w 15VK173   568  C~2nwH      
2015 12  06.39016  03 06 51.165  +15 03 54.87  24.7w 15VK173   568  C~2nwH      
2015 12  13.38310  03 06 22.660  +15 02 27.08  24.4w 15VK173   568  C~2nwH      
2016 01  01.37764  03 05 19.485  +14 59 37.88  24.3w 15VK173   568  C~2nwH      
2016 01  07.32440  03 05 04.985  +14 59 09.19  24.6w 15VK173   568  C~2nwH      
2016 02  04.30735  03 04 37.848  +14 59 54.88  24.9w 15VK173   568  C~2nwH      
2016 02  04.31413  03 04 37.796  +14 59 54.73  24.8w 15VK173   568  C~2nwH      
2016 02  04.32117  03 04 37.817  +14 59 54.86  24.6w 15VK173   568  C~2nwH      
2016 02  04.32803  03 04 37.827  +14 59 54.90  24.6w 15VK173   568  C~2nwH      
2016 02  05.26985  03 04 38.162  +15 00 01.78  24.9w 15VK173   568  C~2nwH      
2016 09  06.59240  03 17 06.472  +15 57 49.03  24.5w 15VK173   568  C~2nwH      
2016 09  26.60468  03 16 22.602  +15 54 56.57  24.3w 15VK173   568  C~2nwH      
2016 10  10.41386  03 15 35.570  +15 51 59.93  24.6w 15VK173   568  C~2nwH      
2016 10  10.47261  03 15 35.350  +15 51 59.14  24.7w 15VK173   568  C~2nwH      
2016 10  27.50838  03 14 23.628  +15 47 38.43  24.5w 15VK173   568  C~2nwH      
2016 11  03.53341  03 13 51.216  +15 45 43.71  24.6w 15VK173   568  C~2nwH      
2016 12  28.40571  03 09 57.853  +15 33 24.67  24.9w 15VK173   568  C~2nwH      
2016 12  29.36323  03 09 55.013  +15 33 17.72  23.7w 15VK173   568  C~2nwH      
2017 01  01.26044  03 09 46.845  +15 32 58.96        15VK173   568  C~2nwH      
2017 01  02.37026  03 09 43.875  +15 32 52.32  24.6w 15VK173   568  C~2nwH      
2017 01  26.26424  03 09 04.962  +15 32 19.34  24.7w 15VK173   568  C~2nwH      
2017 09  15.60092  03 21 21.618  +16 29 08.73  24.5w 15VK173   568  C~2nwH      
2017 09  22.58685  03 21 05.534  +16 28 09.47  24.7w 15VK173   568  C~2nwH      
2017 12  16.38250  03 15 10.806  +16 08 21.98  24.6w 15VK173   568  C~2nwH      
2017 12  16.38715  03 15 10.784  +16 08 21.79  24.3w 15VK173   568  C~2nwH      

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   0.7864   8686.57    -0.00     791.48     0.06
     3   0.8026   8539.25     0.01     788.37     0.13
     4   0.8708   7478.20     0.05     788.36    -0.02
     5   0.8736   7422.52    -0.06     789.03     0.08
     6   0.8737   7419.28     0.06     789.01    -0.00
     7   0.9555   5484.07     0.03     830.82    -0.03
     8   0.9556   5481.04     0.01     830.97     0.01
     9   0.9557   5478.02     0.01     831.09     0.02
    10   0.9641   5260.17    -0.07     838.47     0.11
    11   0.9829   4777.51     0.00     856.54     0.04
    12   0.9830   4774.12    -0.06     856.73     0.08
    13   1.0349   3500.15     0.06     921.00    -0.05
    14   1.0541   3078.89     0.25     949.67    -0.01
    15   1.1061   2152.20     0.03    1038.43     0.05
    16   1.1224   1942.31     0.01    1068.72    -0.10
    17   1.1990   1576.93 (   0.47)   1221.09 (  -0.09)
    18   1.1990   1576.17    -0.33    1221.15    -0.06
    19   1.1990   1576.50    -0.04    1221.19    -0.06
    20   1.1990   1576.65     0.07    1221.19    -0.10
    21   1.2016   1583.21     0.04    1226.47    -0.06
    22   1.7884  12951.67    -0.03    1655.32    -0.04
    23   1.8432  12293.36    -0.06    1654.93    -0.08
    24   1.8810  11589.90    -0.04    1663.16    -0.02
    25   1.8811  11586.62     0.09    1663.24    -0.02
    26   1.9278  10516.40    -0.01    1685.50    -0.06
    27   1.9470  10033.67    -0.02    1699.08    -0.00
    28   2.0973   6582.64    -0.07    1890.17    -0.02
    29   2.0999   6541.20    -0.10    1894.57    -0.09
    30   2.1078   6422.37     0.07    1908.41     0.09
    31   2.1108   6379.21     0.10    1913.62    -0.04
    32   2.1763   5828.46     0.05    2034.16     0.04
    33   2.8124  17010.44     0.06    2520.07    -0.03
    34   2.8315  16770.01    -0.06    2522.22    -0.01
    35   3.0636  11504.92     0.04    2706.37     0.16
    36   3.0637  11504.56    -0.04    2706.27     0.04

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.

15VK173    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        44.080    44.093    44.067
ecceobj         0.059     0.060     0.058
incobj         11.657    11.657    11.657
qmin           40.611    40.611    40.351
qmax           47.107    47.198    47.425
amean          43.764    43.776    43.729
amin           43.426    43.433    43.346
amax           44.123    44.132    44.098
emean           0.052     0.054     0.053
emin            0.036     0.039     0.031
emax            0.068     0.070     0.076
imean          10.247    10.227    10.186
imin            9.717     9.657     9.539
imax           10.781    10.766    10.767
excite_mean     0.185     0.186     0.185
fracstop        1.000     1.000     1.000
cjmean          3.057     3.058     3.057

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       179.6     179.3     179.4
kozaiamp        179.9     180.0     180.0