Orbit Fit and Astrometric record for 15VL169

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: 15VL169   
# Created Wed Dec 25 02:10:31 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     35 observations of     35
# Arc:   6.31y
# First observation: 2015/08/11
#  Last observation: 2021/12/01
# Chi-squared of fit:    13.47 DOF:     64 RMS:  0.11
# Min/Max residuals:    -0.39    0.36
# Exact a, adot, b, bdot, g, gdot:
  1.418693E-05  1.898279E-02  1.944073E-06  2.211647E-03  2.134050E-02 -1.437411E-03
# Covariance matrix:
  1.4563E-13 -3.4542E-14  4.6995E-15 -4.0097E-15  8.3564E-14 -2.8859E-13
 -3.4542E-14  2.2134E-13 -1.0124E-14  2.8016E-14  1.1408E-13  2.0542E-12
  4.6995E-15 -1.0124E-14  5.8639E-14 -1.7091E-14 -1.4397E-15 -1.0476E-13
 -4.0097E-15  2.8016E-14 -1.7091E-14  1.7799E-14  1.3819E-14  2.7927E-13
  8.3564E-14  1.1408E-13 -1.4397E-15  1.3819E-14  1.6549E-13  1.0192E-12
 -2.8859E-13  2.0542E-12 -1.0476E-13  2.7927E-13  1.0192E-12  2.0470E-11
#      lat0       lon0       xBary       yBary       zBary        JD0
   -2.576440   49.593127    1.015718    0.000934    0.017915  2457246.131409
# Heliocentric elements and errors
Epoch:              2457246.5000  =  2015/08/12
Mean Anomaly:          251.44765 +/-     0.057
Argument of Peri:       98.40009 +/-     0.052
Long of Asc Node:       69.57570 +/-     0.001
Inclination:             7.08695 +/-     0.000
Eccentricity:         0.10840636 +/-    0.0002
Semi-Major Axis:     44.85497198 +/-    0.0029
Time of Perihelion: 2490333.0176 +/-      19.0
Perihelion:          39.99240772 +/-    0.0097
Aphelion:            49.71753625 +/-    0.0099
Period (y)              300.4167 +/-      0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           31.10177076 +/-    0.0006
Ecliptic Y           34.97332330 +/-    0.0007
Ecliptic Z           -2.10630866 +/-    0.0000
Ecliptic XDOT        -0.00196765 +/-    0.0000
Ecliptic YDOT         0.00144172 +/-    0.0000
Ecliptic ZDOT         0.00029180 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   46.84971900 +/-    0.0006
Geocenter to KBO     46.85933970 +/-    0.0009
# Hcoef:  7.40

The following table shows the complete astrometric record for 15VL169. 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 (15VL169) followed by the observatory code and reference code for the source of the astrometry.

2015 08  11.63062  03 11 27.755  +15 08 59.07  24.0w 15VL169   568  C~2nw2      
2015 08  12.57765  03 11 28.458  +15 09 00.21  24.2w 15VL169   568  C~2nw2      
2015 09  07.53691  03 11 19.029  +15 07 27.57  24.7w 15VL169   568  C~2nw2      
2015 09  12.53366  03 11 10.890  +15 06 45.61  24.1w 15VL169   568  C~2nw2      
2015 10  07.47747  03 10 03.486  +15 01 41.31  24.1w 15VL169   568  C~2nw2      
2015 10  08.48165  03 09 59.959  +15 01 26.39  24.2w 15VL169   568  C~2nw2      
2015 10  08.53987  03 09 59.737  +15 01 25.35  24.4w 15VL169   568  C~2nw2      
2015 10  08.55151  03 09 59.699  +15 01 25.15  24.6w 15VL169   568  C~2nw2      
2015 10  08.56473  03 09 59.674  +15 01 25.05  24.7w 15VL169   568  C~2nw2      
2015 11  06.29678  03 08 01.795  +14 53 29.50  23.6r 15VL169   568  C~2nw2      
2015 11  06.36009  03 08 01.511  +14 53 28.43  24.0r 15VL169   568  C~2nw2      
2015 11  06.43072  03 08 01.194  +14 53 27.28  23.9r 15VL169   568  C~2nw2      
2015 11  06.50005  03 08 00.872  +14 53 25.99  23.8r 15VL169   568  C~2nw2      
2015 11  07.51946  03 07 56.315  +14 53 08.44  24.1w 15VL169   568  C~2nw2      
2015 11  17.28542  03 07 12.551  +14 50 22.85  24.1w 15VL169   568  C~2nw2      
2015 11  17.33469  03 07 12.324  +14 50 22.04  24.1w 15VL169   568  C~2nw2      
2015 12  13.34802  03 05 23.909  +14 44 00.92  24.5w 15VL169   568  C~2nw2      
2015 12  13.40657  03 05 23.684  +14 44 00.14  24.1w 15VL169   568  C~2nw2      
2016 01  01.40134  03 04 24.076  +14 41 04.01  24.3w 15VL169   568  C~2nw2      
2016 01  07.34755  03 04 10.432  +14 40 32.48  24.7w 15VL169   568  C~2nw2      
2016 09  06.61716  03 15 34.326  +15 32 20.40        15VL169   568  C~2nw2      
2016 09  26.60468  03 14 52.185  +15 29 05.39  24.3w 15VL169   568  C~2nw2      
2016 10  10.41386  03 14 07.281  +15 25 56.80  24.3w 15VL169   568  C~2nw2      
2016 10  10.47261  03 14 07.065  +15 25 55.90  24.3w 15VL169   568  C~2nw2      
2016 10  27.50838  03 12 58.800  +15 21 24.54  24.5w 15VL169   568  C~2nw2      
2016 11  03.53341  03 12 27.998  +15 19 26.42  24.1w 15VL169   568  C~2nw2      
2016 12  28.40571  03 08 46.948  +15 06 51.62  24.5w 15VL169   568  C~2nw2      
2016 12  29.36323  03 08 44.268  +15 06 44.43  24.5w 15VL169   568  C~2nw2      
2017 01  01.26044  03 08 36.562  +15 06 24.71  24.6w 15VL169   568  C~2nw2      
2017 01  02.37026  03 08 33.756  +15 06 17.68  24.4w 15VL169   568  C~2nw2      
2017 01  26.25843  03 07 57.299  +15 05 33.50  24.3w 15VL169   568  C~2nw2      
2017 01  26.26424  03 07 57.293  +15 05 33.53  24.2w 15VL169   568  C~2nw2      
2021 12  01.238290 03 32 19.413  +17 16 06.99  24.4G 15VL169   G37  C~5J85      
2021 12  01.287390 03 32 19.192  +17 16 06.60        15VL169   G37  C~5J85      
2021 12  01.338420 03 32 18.995  +17 16 05.42        15VL169   G37  C~5J85      

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    -0.01       0.00    -0.07
     2   0.0026      0.00    -0.39       0.00     0.24
     3   0.0737      0.00    -0.05       0.00     0.07
     4   0.0873      0.00     0.05       0.00    -0.00
     5   0.1556      0.00     0.07       0.00    -0.02
     6   0.1584      0.00     0.03       0.00     0.04
     7   0.1585      0.00    -0.14       0.00    -0.13
     8   0.1586      0.00    -0.08       0.00    -0.15
     9   0.1586      0.00     0.27       0.00    -0.05
    10   0.2373      0.00     0.01       0.00     0.04
    11   0.2375      0.00     0.05       0.00     0.04
    12   0.2376      0.00     0.10       0.00     0.10
    13   0.2378      0.00    -0.01       0.00     0.01
    14   0.2406      0.00    -0.03       0.00     0.00
    15   0.2674      0.00     0.02       0.00     0.01
    16   0.2675      0.00    -0.04       0.00     0.01
    17   0.3387      0.00     0.16       0.00     0.02
    18   0.3389      0.00     0.09       0.00    -0.05
    19   0.3909      0.00    -0.10       0.00    -0.03
    20   0.4072      0.00     0.02       0.00    -0.08
    21   1.0732      0.00     0.06       0.00    -0.04
    22   1.1279      0.00    -0.01       0.00    -0.03
    23   1.1657      0.00     0.06       0.00     0.03
    24   1.1659      0.00     0.10       0.00    -0.00
    25   1.2125      0.00     0.09       0.00     0.05
    26   1.2318      0.00     0.01       0.00     0.03
    27   1.3820      0.00    -0.06       0.00    -0.05
    28   1.3846      0.00    -0.08       0.00    -0.07
    29   1.3926      0.00    -0.00       0.00     0.12
    30   1.3956      0.00    -0.03       0.00    -0.01
    31   1.4610      0.00     0.02       0.00    -0.02
    32   1.4610      0.00    -0.02       0.00     0.00
    33   6.3069      0.00    -0.21       0.00    -0.03
    34   6.3071      0.00    -0.17       0.00     0.26
    35   6.3072      0.00     0.36       0.00    -0.22

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.

15VL169    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        45.240    45.240    45.240
ecceobj         0.100     0.100     0.100
incobj          7.069     7.069     7.069
qmin           39.354    39.354    39.369
qmax           50.825    50.766    50.797
amean          44.936    44.936    44.936
amin           44.563    44.576    44.569
amax           45.348    45.328    45.339
emean           0.106     0.106     0.106
emin            0.092     0.092     0.092
emax            0.121     0.121     0.120
imean           5.607     5.607     5.607
imin            5.010     5.010     5.009
imax            6.199     6.198     6.198
excite_mean     0.144     0.144     0.144
fracstop        1.000     1.000     1.000
cjmean          3.088     3.088     3.088

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       186.0     186.0     186.0
kozaiamp        179.9     180.0     179.9