Orbit Fit and Astrometric record for 15VB169

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: 15VB169   
# Created Tue Apr  1 01:10:40 2025
# Orbit generated from Bernstein formalism
# Fitting     38 observations of     38
# Arc:   3.08y
# First observation: 2014/11/17
#  Last observation: 2017/12/16
Preliminary a, adot, b, bdot, g, gdot:
  -0.000014   0.018706  -0.000002   0.000367   0.021362   0.000000
# Chi-squared of fit:     7.63 DOF:     70 RMS:  0.08
# Min/Max residuals:    -0.19    0.21
# Exact a, adot, b, bdot, g, gdot:
  1.367505E-05  1.879651E-02 -1.650376E-07  3.691031E-04  2.148824E-02  1.358814E-04
# Covariance matrix:
  2.8836E-13 -3.1174E-13  2.8565E-15 -4.6187E-15 -1.4983E-13 -3.9485E-12
 -3.1174E-13  4.6977E-13 -5.1870E-15  8.5170E-15  2.6205E-13  7.2556E-12
  2.8565E-15 -5.1870E-15  1.6793E-13 -9.1341E-14 -3.8412E-15 -9.2868E-14
 -4.6187E-15  8.5170E-15 -9.1341E-14  6.4807E-14  5.2653E-15  1.5254E-13
 -1.4983E-13  2.6205E-13 -3.8412E-15  5.2653E-15  2.7453E-13  4.6876E-12
 -3.9485E-12  7.2556E-12 -9.2868E-14  1.5254E-13  4.6876E-12  1.2994E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
   -1.785806   47.622272   -0.119973   -0.030450   -0.981686  2456978.901288
# Heliocentric elements and errors
Epoch:              2456970.5000  =  2014/11/09
Mean Anomaly:          174.43036 +/-     0.402
Argument of Peri:      127.53201 +/-     0.403
Long of Asc Node:      104.96676 +/-     0.018
Inclination:             2.08054 +/-     0.000
Eccentricity:         0.07907677 +/-    0.0001
Semi-Major Axis:     44.04869661 +/-    0.0026
Time of Perihelion: 2512013.5449 +/-     119.3
Perihelion:          40.56546817 +/-    0.0036
Aphelion:            47.53192506 +/-    0.0039
Period (y)              292.3532 +/-      0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           31.92170530 +/-    0.0008
Ecliptic Y           35.16896620 +/-    0.0008
Ecliptic Z           -1.45027456 +/-    0.0000
Ecliptic XDOT        -0.00176077 +/-    0.0000
Ecliptic YDOT         0.00162309 +/-    0.0000
Ecliptic ZDOT         0.00004657 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   47.51794134 +/-    0.0008
Geocenter to KBO     46.53707993 +/-    0.0011
# Hcoef:  7.66

The following table shows the complete astrometric record for 15VB169. 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 (15VB169) followed by the observatory code and reference code for the source of the astrometry.

2014 11  17.40051  03 02 42.752  +15 22 24.68  24.3r 15VB169   568  C~2nw0      
2014 11  17.51464  03 02 42.250  +15 22 22.60  24.2r 15VB169   568  C~2nw0      
2014 11  19.30670  03 02 34.427  +15 21 50.93  24.2r 15VB169   568  C~2nw0      
2014 11  23.41007  03 02 16.685  +15 20 39.45  23.6r 15VB169   568  C~2nw0      
2015 08  11.62323  03 11 12.604  +16 00 28.51  24.6w 15VB169   568  C~2nw0      
2015 09  07.53281  03 11 04.026  +15 58 59.29  24.4w 15VB169   568  C~2nw0      
2015 09  12.52956  03 10 55.983  +15 58 17.86  24.1w 15VB169   568  C~2nw0      
2015 10  07.47166  03 09 49.375  +15 53 12.24  24.8w 15VB169   568  C~2nw0      
2015 11  06.29151  03 07 49.190  +15 44 47.43  24.4r 15VB169   568  C~2nw0      
2015 11  06.42547  03 07 48.611  +15 44 45.38  24.2r 15VB169   568  C~2nw0      
2015 11  06.49480  03 07 48.286  +15 44 43.90  24.4r 15VB169   568  C~2nw0      
2015 11  07.51356  03 07 43.802  +15 44 25.67  24.7w 15VB169   568  C~2nw0      
2015 11  17.27960  03 07 00.599  +15 41 31.88  24.5w 15VB169   568  C~2nw0      
2015 11  17.32888  03 07 00.381  +15 41 31.05  24.5w 15VB169   568  C~2nw0      
2015 12  06.40765  03 05 39.764  +15 36 17.18  24.3w 15VB169   568  C~2nw0      
2015 12  13.34220  03 05 13.409  +15 34 38.39  24.2w 15VB169   568  C~2nw0      
2015 12  13.40075  03 05 13.190  +15 34 37.57  24.7w 15VB169   568  C~2nw0      
2016 01  01.39556  03 04 14.482  +15 31 09.72  25.2w 15VB169   568  C~2nw0      
2016 01  07.34177  03 04 01.054  +15 30 27.31  24.4w 15VB169   568  C~2nw0      
2016 02  04.27190  03 03 36.373  +15 29 53.82  24.8w 15VB169   568  C~2nw0      
2016 02  10.26162  03 03 39.841  +15 30 23.54  23.9w 15VB169   568  C~2nw0      
2016 09  07.55050  03 15 17.248  +16 17 03.01        15VB169   568  C~2nw0      
2016 09  26.61279  03 14 36.905  +16 13 52.88  24.5w 15VB169   568  C~2nw0      
2016 10  10.42589  03 13 52.595  +16 10 41.09  26.3w 15VB169   568  C~2nw0      
2016 10  10.48430  03 13 52.390  +16 10 40.12  25.0w 15VB169   568  C~2nw0      
2016 10  10.50790  03 13 52.303  +16 10 39.77  24.8w 15VB169   568  C~2nw0      
2016 10  27.50838  03 12 45.137  +16 06 01.87  24.8w 15VB169   568  C~2nw0      
2016 10  27.51417  03 12 45.119  +16 06 01.86  24.7w 15VB169   568  C~2nw0      
2016 11  03.53341  03 12 14.794  +16 03 59.67  24.6w 15VB169   568  C~2nw0      
2016 11  03.53920  03 12 14.768  +16 03 59.55  24.8w 15VB169   568  C~2nw0      
2016 12  29.36878  03 08 34.571  +15 50 13.11  24.9w 15VB169   568  C~2nw0      
2017 01  01.26608  03 08 27.002  +15 49 48.28  24.7w 15VB169   568  C~2nw0      
2017 01  02.37586  03 08 24.228  +15 49 39.47  25.0w 15VB169   568  C~2nw0      
2017 01  26.26424  03 07 48.549  +15 48 10.75  24.7w 15VB169   568  C~2nw0      
2017 01  26.27054  03 07 48.545  +15 48 10.73  24.5w 15VB169   568  C~2nw0      
2017 09  15.60092  03 19 19.269  +16 33 49.36  24.7w 15VB169   568  C~2nw0      
2017 09  22.58685  03 19 04.007  +16 32 39.48  24.4w 15VB169   568  C~2nw0      
2017 12  16.38715  03 13 31.903  +16 11 01.97  24.7w 15VB169   568  C~2nw0      

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     0.09
     2   0.0003     -7.55     0.10       0.02     0.03
     3   0.0052   -125.05    -0.02       1.07     0.09
     4   0.0165   -391.43     0.05       3.86    -0.04
     5   0.7316   7710.16    -0.05     184.96     0.01
     6   0.8053   7566.86    -0.04     132.18    -0.05
     7   0.8190   7443.85     0.07     123.43     0.04
     8   0.8873   6435.14    -0.14      87.89    -0.02
     9   0.9689   4627.41    -0.19      72.32    -0.07
    10   0.9693   4618.80     0.18      72.62     0.17
    11   0.9695   4613.88    -0.09      72.47    -0.00
    12   0.9722   4546.59     0.07      72.57    -0.01
    13   0.9990   3898.76     0.07      75.56    -0.06
    14   0.9991   3895.50     0.11      75.62    -0.04
    15   1.0514   2689.32     0.02      92.81    -0.07
    16   1.0703   2296.00    -0.01     102.54     0.01
    17   1.0705   2292.73    -0.04     102.62    -0.01
    18   1.1225   1419.84    -0.06     136.82    -0.15
    19   1.1388   1221.59    -0.03     149.72     0.05
    20   1.2153    869.51    -0.19     216.30    -0.00
    21   1.2317    925.91    -0.12     230.97    -0.17
    22   1.8074  11380.55     0.09     205.97     0.02
    23   1.8596  10768.26    -0.05     175.92     0.15
    24   1.8974  10100.31    -0.07     160.00     0.12
    25   1.8976  10097.20     0.03     159.85    -0.00
    26   1.8976  10095.89     0.03     159.85     0.00
    27   1.9442   9086.87    -0.05     149.33    -0.05
    28   1.9442   9086.62     0.07     149.39     0.01
    29   1.9634   8631.95     0.02     148.28    -0.02
    30   1.9634   8631.56     0.01     148.27    -0.04
    31   2.1163   5346.72     0.16     207.69     0.05
    32   2.1242   5234.79     0.21     213.45    -0.04
    33   2.1272   5193.84    -0.08     215.84     0.03
    34   2.1926   4673.90     0.01     270.52    -0.00
    35   2.1927   4673.84     0.00     270.52    -0.02
    36   2.8287  15019.65    -0.06     267.90    -0.02
    37   2.8479  14788.39    -0.02     257.20    -0.04
    38   3.0800   9817.81    -0.02     259.39     0.07

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.

15VB169    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        44.359    44.367    44.351
ecceobj         0.073     0.073     0.073
incobj          2.082     2.082     2.082
qmin           39.982    39.994    39.960
qmax           48.378    48.365    48.347
amean          44.065    44.073    44.058
amin           43.709    43.726    43.706
amax           44.447    44.436    44.424
emean           0.073     0.073     0.073
emin            0.056     0.056     0.057
emax            0.089     0.089     0.089
imean           0.788     0.785     0.791
imin            0.020     0.020     0.020
imax            1.353     1.350     1.357
excite_mean     0.074     0.074     0.075
fracstop        1.000     1.000     1.000
cjmean          3.096     3.096     3.095

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       178.1     178.3     177.8
kozaiamp        180.0     180.0     180.0