Orbit Fit and Astrometric record for 15VF169

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: 15VF169   
# Created Sun Nov 24 02:10:32 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     43 observations of     43
# Arc:   8.11y
# First observation: 2014/11/17
#  Last observation: 2022/12/26
# Chi-squared of fit:    10.36 DOF:     80 RMS:  0.09
# Min/Max residuals:    -0.22    0.26
# Exact a, adot, b, bdot, g, gdot:
  1.475176E-05  2.118256E-02  6.439148E-07  6.353975E-04  2.283328E-02  1.133464E-03
# Covariance matrix:
  1.9379E-13 -1.5809E-13  4.4621E-15 -4.5380E-15 -5.1343E-14 -8.3903E-13
 -1.5809E-13  1.6274E-13 -4.7652E-15  4.9843E-15  4.2526E-14  9.1870E-13
  4.4621E-15 -4.7652E-15  6.5665E-14 -2.0688E-14 -1.9416E-15 -2.8950E-14
 -4.5380E-15  4.9843E-15 -2.0688E-14  1.3790E-14  8.9187E-16  3.1080E-14
 -5.1343E-14  4.2526E-14 -1.9416E-15  8.9187E-16  1.1883E-13  1.8721E-13
 -8.3903E-13  9.1870E-13 -2.8950E-14  3.1080E-14  1.8721E-13  5.7126E-12
#      lat0       lon0       xBary       yBary       zBary        JD0
   -2.751365   46.503509   -0.137143   -0.046891   -0.978802  2456978.787348
# Heliocentric elements and errors
Epoch:              2456978.5000  =  2014/11/17
Mean Anomaly:          107.90111 +/-     0.083
Argument of Peri:      188.48856 +/-     0.077
Long of Asc Node:      104.09411 +/-     0.005
Inclination:             3.19315 +/-     0.000
Eccentricity:         0.05784310 +/-    0.0001
Semi-Major Axis:     43.86460075 +/-    0.0028
Time of Perihelion: 2425173.6678 +/-      24.7
Perihelion:          41.32733622 +/-    0.0048
Aphelion:            46.40186527 +/-    0.0050
Period (y)              290.5223 +/-      0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           30.68217027 +/-    0.0005
Ecliptic Y           32.54029407 +/-    0.0005
Ecliptic Z           -2.10226519 +/-    0.0000
Ecliptic XDOT        -0.00175082 +/-    0.0000
Ecliptic YDOT         0.00184442 +/-    0.0000
Ecliptic ZDOT         0.00006968 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   44.77368342 +/-    0.0005
Geocenter to KBO     43.79572095 +/-    0.0007
# Hcoef:  7.75

The following table shows the complete astrometric record for 15VF169. 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 (15VF169) followed by the observatory code and reference code for the source of the astrometry.

2014 11  17.28657  02 59 23.570  +14 08 00.29  24.3r 15VF169   568  C~2nw1      
2014 11  17.39535  02 59 23.060  +14 07 58.39  24.3r 15VF169   568  C~2nw1      
2014 11  17.50914  02 59 22.534  +14 07 56.27  24.2r 15VF169   568  C~2nw1      
2014 11  19.30032  02 59 14.398  +14 07 23.25  24.2r 15VF169   568  C~2nw1      
2014 11  23.40372  02 58 55.900  +14 06 09.34  24.2r 15VF169   568  C~2nw1      
2015 08  11.63062  03 08 35.664  +14 51 51.30  24.1w 15VF169   568  C~2nw1      
2015 09  07.53691  03 08 26.148  +14 49 43.74  24.5w 15VF169   568  C~2nw1      
2015 09  12.53366  03 08 17.594  +14 48 53.83  24.5w 15VF169   568  C~2nw1      
2015 10  07.47747  03 07 07.249  +14 43 05.11  24.3w 15VF169   568  C~2nw1      
2015 10  08.48165  03 07 03.581  +14 42 48.11  24.5w 15VF169   568  C~2nw1      
2015 10  08.53987  03 07 03.349  +14 42 47.04  24.4w 15VF169   568  C~2nw1      
2015 10  08.55151  03 07 03.311  +14 42 46.97  24.5w 15VF169   568  C~2nw1      
2015 10  08.56473  03 07 03.260  +14 42 46.71  24.7w 15VF169   568  C~2nw1      
2015 11  06.29678  03 05 01.082  +14 33 56.87  24.2r 15VF169   568  C~2nw1      
2015 11  06.36009  03 05 00.796  +14 33 55.56  24.4r 15VF169   568  C~2nw1      
2015 11  06.43072  03 05 00.433  +14 33 54.25  24.1r 15VF169   568  C~2nw1      
2015 11  06.50005  03 05 00.136  +14 33 52.83  24.5r 15VF169   568  C~2nw1      
2015 11  07.51946  03 04 55.417  +14 33 33.61  24.4w 15VF169   568  C~2nw1      
2015 11  17.29127  03 04 10.252  +14 30 30.71  24.4w 15VF169   568  C~2nw1      
2015 11  17.34053  03 04 10.022  +14 30 29.86  24.3w 15VF169   568  C~2nw1      
2015 12  13.34802  03 02 18.945  +14 23 30.24  24.5w 15VF169   568  C~2nw1      
2015 12  13.35388  03 02 18.918  +14 23 30.18  24.4w 15VF169   568  C~2nw1      
2015 12  13.40657  03 02 18.719  +14 23 29.48  24.3w 15VF169   568  C~2nw1      
2015 12  13.41241  03 02 18.693  +14 23 29.36  24.4w 15VF169   568  C~2nw1      
2016 01  01.40134  03 01 18.510  +14 20 14.21  24.5w 15VF169   568  C~2nw1      
2016 01  07.34755  03 01 04.956  +14 19 38.63  24.7w 15VF169   568  C~2nw1      
2016 02  04.27768  03 00 41.924  +14 19 54.80  24.5w 15VF169   568  C~2nw1      
2016 02  10.26747  03 00 46.219  +14 20 38.21  24.6w 15VF169   568  C~2nw1      
2016 09  06.61716  03 13 08.997  +15 11 08.17        15VF169   568  C~2nw1      
2016 09  26.60468  03 12 25.166  +15 07 19.14  23.4w 15VF169   568  C~2nw1      
2016 10  10.41386  03 11 38.593  +15 03 45.00  24.6w 15VF169   568  C~2nw1      
2016 10  10.47261  03 11 38.366  +15 03 44.07  24.7w 15VF169   568  C~2nw1      
2016 10  27.51997  03 10 27.725  +14 58 40.84  24.5w 15VF169   568  C~2nw1      
2016 10  27.53156  03 10 27.667  +14 58 40.61  24.6w 15VF169   568  C~2nw1      
2016 11  03.54499  03 09 55.950  +14 56 30.00  24.1w 15VF169   568  C~2nw1      
2016 11  03.55656  03 09 55.899  +14 56 29.82  24.3w 15VF169   568  C~2nw1      
2016 12  28.38265  03 06 10.082  +14 42 41.58  25.1w 15VF169   568  C~2nw1      
2016 12  29.34821  03 06 07.367  +14 42 33.50        15VF169   568  C~2nw1      
2017 01  01.24491  03 05 59.630  +14 42 11.31  23.9w 15VF169   568  C~2nw1      
2017 01  02.35523  03 05 56.832  +14 42 03.86  24.5w 15VF169   568  C~2nw1      
2017 01  26.25843  03 05 21.409  +14 41 10.09  24.2w 15VF169   568  C~2nw1      
2022 12  26.103920 03 34 47.068  +16 46 46.24  24.9G 15VF169   G37  C~69cT      
2022 12  26.218870 03 34 46.628  +16 46 45.40        15VF169   G37  C~69cT      

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    -0.05
     2   0.0003      0.00    -0.08       0.00     0.06
     3   0.0006      0.00    -0.04       0.00     0.06
     4   0.0055      0.00     0.08       0.00     0.04
     5   0.0167      0.00    -0.04       0.00     0.04
     6   0.7319      0.00    -0.07       0.00     0.11
     7   0.8056      0.00    -0.01       0.00     0.06
     8   0.8193      0.00    -0.03       0.00     0.07
     9   0.8876      0.00     0.02       0.00     0.08
    10   0.8903      0.00     0.01       0.00    -0.04
    11   0.8905      0.00    -0.18       0.00    -0.13
    12   0.8905      0.00    -0.09       0.00    -0.00
    13   0.8906      0.00    -0.11       0.00    -0.04
    14   0.9692      0.00     0.11       0.00    -0.00
    15   0.9694      0.00     0.26       0.00    -0.12
    16   0.9696      0.00    -0.22       0.00    -0.09
    17   0.9698      0.00     0.20       0.00    -0.18
    18   0.9726      0.00     0.01       0.00    -0.01
    19   0.9993      0.00     0.07       0.00     0.00
    20   0.9995      0.00     0.07       0.00     0.05
    21   1.0707      0.00     0.05       0.00     0.02
    22   1.0707      0.00    -0.01       0.00     0.04
    23   1.0708      0.00     0.03       0.00     0.04
    24   1.0708      0.00    -0.02       0.00     0.00
    25   1.1228      0.00    -0.09       0.00     0.01
    26   1.1391      0.00     0.04       0.00     0.10
    27   1.2156      0.00     0.04       0.00     0.01
    28   1.2320      0.00     0.09       0.00    -0.10
    29   1.8051      0.00     0.01       0.00    -0.02
    30   1.8599      0.00     0.09       0.00     0.11
    31   1.8977      0.00     0.02       0.00     0.01
    32   1.8978      0.00     0.00       0.00     0.06
    33   1.9445      0.00     0.05       0.00     0.04
    34   1.9445      0.00    -0.04       0.00     0.03
    35   1.9637      0.00     0.06       0.00    -0.03
    36   1.9638      0.00     0.11       0.00     0.01
    37   2.1139      0.00    -0.04       0.00     0.03
    38   2.1165      0.00    -0.03       0.00    -0.07
    39   2.1245      0.00    -0.10       0.00    -0.21
    40   2.1275      0.00     0.03       0.00     0.02
    41   2.1929      0.00    -0.04       0.00     0.00
    42   8.1063      0.00     0.18       0.00    -0.11
    43   8.1066      0.00    -0.21       0.00     0.15

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.

15VF169    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        44.212    44.212    44.212
ecceobj         0.060     0.060     0.060
incobj          3.195     3.195     3.195
qmin           40.613    40.615    40.611
qmax           47.372    47.363    47.379
amean          43.889    43.889    43.889
amin           43.539    43.542    43.542
amax           44.249    44.256    44.252
emean           0.054     0.054     0.054
emin            0.037     0.037     0.037
emax            0.071     0.071     0.071
imean           1.618     1.618     1.618
imin            0.888     0.888     0.888
imax            2.238     2.238     2.238
excite_mean     0.062     0.062     0.062
fracstop        1.000     1.000     1.000
cjmean          3.096     3.096     3.096

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       170.4     170.1     170.3
kozaiamp        180.0     180.0     180.0