Orbit Fit and Astrometric record for 14VV39

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: 14VV39    
# Created Sun Nov 24 02:10:06 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     65 observations of     65
# Arc:  11.06y
# First observation: 2013/09/11
#  Last observation: 2024/10/01
# Chi-squared of fit:    14.99 DOF:    124 RMS:  0.08
# Min/Max residuals:    -0.23    0.32
# Exact a, adot, b, bdot, g, gdot:
  1.501445E-05  2.245612E-02 -1.146967E-06 -3.961089E-04  2.347218E-02 -6.193030E-05
# Covariance matrix:
  1.3642E-13 -2.9499E-14 -7.9915E-16  3.7730E-16  9.1023E-14 -7.9187E-14
 -2.9499E-14  1.6184E-14  3.4670E-16 -2.5349E-16 -5.3800E-15  5.9083E-14
 -7.9915E-16  3.4670E-16  4.5005E-14 -7.2317E-15 -4.9305E-16  1.4090E-15
  3.7730E-16 -2.5349E-16 -7.2317E-15  2.3253E-15  5.4012E-17 -1.0888E-15
  9.1023E-14 -5.3800E-15 -4.9305E-16  5.4012E-17  1.2406E-13  3.7293E-16
 -7.9187E-14  5.9083E-14  1.4090E-15 -1.0888E-15  3.7293E-16  2.5625E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
   -1.297672    7.971734    0.337450   -0.021399   -0.949055  2456546.803658
# Heliocentric elements and errors
Epoch:              2456546.5000  =  2013/09/11
Mean Anomaly:          308.47676 +/-     0.146
Argument of Peri:      284.20976 +/-     0.152
Long of Asc Node:      136.33048 +/-     0.004
Inclination:             1.62867 +/-     0.000
Eccentricity:         0.01623543 +/-    0.0000
Semi-Major Axis:     43.99120166 +/-    0.0028
Time of Perihelion: 2471799.2391 +/-      44.1
Perihelion:          43.27698570 +/-    0.0030
Aphelion:            44.70541762 +/-    0.0031
Period (y)              291.7810 +/-      0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           43.16765172 +/-    0.0006
Ecliptic Y            5.70751702 +/-    0.0001
Ecliptic Z           -0.96490340 +/-    0.0000
Ecliptic XDOT        -0.00037763 +/-    0.0000
Ecliptic YDOT         0.00259171 +/-    0.0000
Ecliptic ZDOT        -0.00004589 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   43.55403154 +/-    0.0006
Geocenter to KBO     42.60366827 +/-    0.0006
# Hcoef:  6.44

The following table shows the complete astrometric record for 14VV39. 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 (14VV39) followed by the observatory code and reference code for the source of the astrometry.

2013 09  11.30288  00 31 20.068  +01 58 11.43  23.2g 14VV39    W84  C~4yV3      
2013 09  11.30288  00 31 20.08   +01 58 11.4   23.6g 14VV39    W84  C~3coU      
2013 09  28.10898  00 30 09.564  +01 50 27.37  23.8g 14VV39    W84  C~4yV3      
2013 09  28.10898  00 30 09.56   +01 50 27.4   23.7g 14VV39    W84  C~3coU      
2013 10  04.15303  00 29 43.453  +01 47 38.33  23.1g 14VV39    W84  C~4yV3      
2013 10  04.15303  00 29 43.45   +01 47 38.3   23.3g 14VV39    W84  C~3coU      
2013 10  13.09336  00 29 05.258  +01 43 33.08  22.1z 14VV39    W84  C~4yV3      
2013 10  13.09336  00 29 05.26   +01 43 33.1   22.1z 14VV39    W84  C~3coU      
2013 10  13.12065  00 29 05.139  +01 43 32.27  22.4i 14VV39    W84  C~4yV3      
2013 10  13.12065  00 29 05.14   +01 43 32.3   22.5i 14VV39    W84  C~3coU      
2013 11  08.17535  00 27 26.408  +01 33 13.35  22.5r 14VV39    W84  C~4yV3      
2013 11  08.17535  00 27 26.41   +01 33 13.4   22.7r 14VV39    W84  C~3coU      
2013 11  08.17673  00 27 26.401  +01 33 13.52  22.2i 14VV39    W84  C~4yV3      
2013 11  08.17673  00 27 26.40   +01 33 13.5   22.4i 14VV39    W84  C~3coU      
2013 11  22.08391  00 26 47.897  +01 29 22.24  23.8g 14VV39    W84  C~4yV3      
2013 11  22.08391  00 26 47.90   +01 29 22.3   23.7g 14VV39    W84  C~3coU      
2013 11  22.09533  00 26 47.869  +01 29 22.14  22.7r 14VV39    W84  C~4yV3      
2013 11  22.09533  00 26 47.87   +01 29 22.1   22.8r 14VV39    W84  C~3coU      
2013 11  22.09673  00 26 47.868  +01 29 22.18  22.7i 14VV39    W84  C~4yV3      
2013 11  22.09673  00 26 47.87   +01 29 22.2   22.8i 14VV39    W84  C~3coU      
2013 11  23.10640  00 26 45.580  +01 29 08.91  22.5i 14VV39    W84  C~4yV3      
2013 11  23.10640  00 26 45.58   +01 29 08.9   22.7i 14VV39    W84  C~3coU      
2014 11  14.05019  00 31 53.553  +02 00 30.09  22.6z 14VV39    W84  C~4yV3      
2014 11  14.05019  00 31 53.55   +02 00 30.1   22.4z 14VV39    W84  C~3coU      
2015 10  17.16393  00 38 22.404  +02 40 13.65  22.9r 14VV39    W84  C~4yV3      
2015 10  17.16393  00 38 22.40   +02 40 13.7   22.9r 14VV39    W84  C~3coU      
2016 09  09.28058  00 45 45.21   +03 26 04.8   22.7r 14VV39    W84  C~3coU      
2016 09  09.28195  00 45 45.19   +03 26 04.8   22.2i 14VV39    W84  C~3coU      
2016 09  09.282789 00 45 45.19   +03 26 05.0   23.4g 14VV39    W84  C~352S      
2016 11  08.11301  00 41 40.332  +03 00 07.61  22.5i 14VV39    W84  C~4yV3      
2016 11  08.11301  00 41 40.33   +03 00 07.6   22.6i 14VV39    W84  C~3coU      
2016 11  08.11440  00 41 40.334  +03 00 07.83  22.6z 14VV39    W84  C~4yV3      
2016 11  18.08408  00 41 09.061  +02 57 00.15  23.0r 14VV39    W84  C~4yV3      
2016 11  18.08408  00 41 09.06   +02 57 00.2   23.1r 14VV39    W84  C~3coU      
2016 11  18.08544  00 41 09.050  +02 57 00.35  24.1g 14VV39    W84  C~4yV3      
2016 11  26.10227  00 40 48.484  +02 55 00.52  23.0r 14VV39    W84  C~4yV3      
2016 11  26.10227  00 40 48.48   +02 55 00.5   22.9r 14VV39    W84  C~3coU      
2016 11  26.10867  00 40 48.471  +02 55 00.46  22.3i 14VV39    W84  C~4yV3      
2016 11  26.10867  00 40 48.47   +02 55 00.5   22.6i 14VV39    W84  C~3coU      
2016 11  30.090868 00 40 39.97   +02 54 12.6   22.3z 14VV39    W84  C~352S      
2016 11  30.09140  00 40 39.974  +02 54 12.54  22.5z 14VV39    W84  C~4yV3      
2017 08  28.276620 00 51 14.60   +03 59 43.4   22.5i 14VV39    W84  C~352S      
2017 08  28.27714  00 51 14.595  +03 59 43.32  22.4i 14VV39    W84  C~4yV3      
2017 08  28.277998 00 51 14.60   +03 59 43.4   22.8r 14VV39    W84  C~352S      
2017 08  28.27853  00 51 14.598  +03 59 43.39  22.8r 14VV39    W84  C~4yV3      
2017 08  28.279375 00 51 14.59   +03 59 43.3   23.6g 14VV39    W84  C~352S      
2017 08  28.27990  00 51 14.593  +03 59 43.24  23.6g 14VV39    W84  C~4yV3      
2017 09  27.227581 00 49 19.48   +03 47 06.4   22.7r 14VV39    W84  C~352S      
2017 09  27.22811  00 49 19.484  +03 47 06.31  22.8r 14VV39    W84  C~4yV3      
2017 09  27.228970 00 49 19.48   +03 47 06.2   22.6i 14VV39    W84  C~352S      
2017 09  27.22950  00 49 19.480  +03 47 06.26  22.6i 14VV39    W84  C~4yV3      
2017 09  27.23087  00 49 19.466  +03 47 06.33  23.6g 14VV39    W84  C~4yV3      
2017 10  20.168542 00 47 40.55   +03 36 39.2   22.1z 14VV39    W84  C~352S      
2017 10  20.16907  00 47 40.550  +03 36 39.29  22.0z 14VV39    W84  C~4yV3      
2017 10  22.196204 00 47 32.07   +03 35 46.4   22.4z 14VV39    W84  C~352S      
2017 10  22.19674  00 47 32.068  +03 35 46.41  22.4z 14VV39    W84  C~4yV3      
2018 10  10.23758  00 53 11.636  +04 10 06.87  22.8r 14VV39    W84  C~4yV3      
2018 10  18.19756  00 52 37.216  +04 06 31.23  22.2z 14VV39    W84  C~4yV3      
2018 10  18.19894  00 52 37.204  +04 06 31.08  22.4i 14VV39    W84  C~4yV3      
2024 10  01.352720 01 22 50.369  +07 05 16.04  22.7G 14VV39    G37  C~8H4c      
2024 10  01.355210 01 22 50.352  +07 05 15.98        14VV39    G37  C~8H4c      
2024 10  01.396240 01 22 50.175  +07 05 14.98        14VV39    G37  C~8H4c      
2024 10  01.398920 01 22 50.162  +07 05 14.90        14VV39    G37  C~8H4c      
2024 10  01.439870 01 22 49.987  +07 05 13.77        14VV39    G37  C~8H4c      
2024 10  01.442410 01 22 49.979  +07 05 13.78        14VV39    G37  C~8H4c      

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    -0.05       0.00     0.18
     2   0.0000      0.00     0.13       0.00     0.15
     3   0.0460      0.00    -0.13       0.00    -0.16
     4   0.0460      0.00    -0.07       0.00    -0.19
     5   0.0626      0.00    -0.06       0.00    -0.00
     6   0.0626      0.00    -0.10       0.00    -0.03
     7   0.0870      0.00     0.08       0.00     0.10
     8   0.0870      0.00     0.05       0.00     0.08
     9   0.0871      0.00     0.03       0.00     0.03
    10   0.0871      0.00     0.02       0.00    -0.00
    11   0.1584      0.00     0.04       0.00    -0.06
    12   0.1584      0.00     0.01       0.00    -0.11
    13   0.1584      0.00    -0.04       0.00     0.06
    14   0.1584      0.00    -0.03       0.00     0.08
    15   0.1965      0.00     0.09       0.00    -0.05
    16   0.1965      0.00     0.04       0.00    -0.11
    17   0.1966      0.00     0.04       0.00    -0.10
    18   0.1966      0.00     0.03       0.00    -0.06
    19   0.1966      0.00     0.09       0.00     0.02
    20   0.1966      0.00     0.06       0.00     0.00
    21   0.1993      0.00     0.05       0.00     0.04
    22   0.1993      0.00     0.05       0.00     0.05
    23   1.1738      0.00    -0.23       0.00    -0.07
    24   1.1738      0.00    -0.19       0.00    -0.08
    25   2.0968      0.00    -0.11       0.00     0.09
    26   2.0968      0.00    -0.05       0.00     0.04
    27   2.9951      0.00     0.08       0.00     0.06
    28   2.9952      0.00    -0.14       0.00     0.10
    29   2.9952      0.00    -0.09       0.00     0.32
    30   3.1590      0.00     0.00       0.00    -0.05
    31   3.1590      0.00     0.03       0.00    -0.04
    32   3.1590      0.00     0.13       0.00     0.21
    33   3.1863      0.00     0.09       0.00    -0.03
    34   3.1863      0.00     0.10       0.00    -0.08
    35   3.1863      0.00    -0.01       0.00     0.14
    36   3.2082      0.00    -0.03       0.00    -0.07
    37   3.2082      0.00     0.03       0.00    -0.05
    38   3.2082      0.00     0.05       0.00     0.01
    39   3.2082      0.00     0.06       0.00    -0.03
    40   3.2191      0.00     0.05       0.00     0.09
    41   3.2191      0.00     0.12       0.00     0.04
    42   3.9616      0.00     0.06       0.00    -0.01
    43   3.9616      0.00     0.01       0.00    -0.08
    44   3.9616      0.00     0.12       0.00     0.02
    45   3.9616      0.00     0.12       0.00     0.02
    46   3.9616      0.00     0.04       0.00    -0.05
    47   3.9616      0.00     0.11       0.00    -0.10
    48   4.0436      0.00    -0.10       0.00     0.08
    49   4.0436      0.00    -0.01       0.00     0.00
    50   4.0436      0.00    -0.01       0.00    -0.08
    51   4.0436      0.00     0.02       0.00    -0.01
    52   4.0436      0.00    -0.10       0.00     0.10
    53   4.1064      0.00    -0.05       0.00    -0.10
    54   4.1064      0.00    -0.02       0.00     0.01
    55   4.1120      0.00    -0.14       0.00    -0.10
    56   4.1120      0.00    -0.13       0.00    -0.08
    57   5.0785      0.00     0.02       0.00    -0.01
    58   5.1003      0.00     0.11       0.00     0.02
    59   5.1003      0.00     0.02       0.00    -0.09
    60  11.0556      0.00     0.05       0.00    -0.04
    61  11.0556      0.00    -0.05       0.00    -0.04
    62  11.0557      0.00    -0.03       0.00     0.04
    63  11.0557      0.00    -0.05       0.00     0.03
    64  11.0558      0.00    -0.02       0.00    -0.03
    65  11.0558      0.00     0.03       0.00     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.

14VV39    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        44.239    44.239    44.239
ecceobj         0.019     0.019     0.019
incobj          1.626     1.626     1.626
qmin           42.211    42.206    42.211
qmax           45.986    45.982    45.989
amean          44.000    44.000    44.000
amin           43.656    43.655    43.656
amax           44.342    44.344    44.341
emean           0.022     0.022     0.022
emin            0.006     0.006     0.006
emax            0.037     0.037     0.037
imean           1.429     1.429     1.429
imin            0.786     0.786     0.786
imax            2.031     2.031     2.031
excite_mean     0.033     0.033     0.033
fracstop        1.000     1.000     1.000
cjmean          3.100     3.100     3.100

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       198.0     198.0     198.0
kozaiamp        179.9     179.9     179.9