Orbit Fit and Astrometric record for 15VV171

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: 15VV171   
# Created Tue Apr  1 01:10:42 2025
# Orbit generated from Bernstein formalism
# Fitting     36 observations of     36
# Arc:   3.08y
# First observation: 2014/11/17
#  Last observation: 2017/12/16
Preliminary a, adot, b, bdot, g, gdot:
  -0.000149   0.025971   0.000004  -0.000841   0.025156   0.000000
# Chi-squared of fit:    13.04 DOF:     66 RMS:  0.11
# Min/Max residuals:    -0.32    0.22
# Exact a, adot, b, bdot, g, gdot:
  1.602809E-05  2.582539E-02 -8.029294E-07 -8.353147E-04  2.512519E-02 -3.506950E-03
# Covariance matrix:
  3.7322E-13 -4.1016E-13 -5.2444E-15  9.8460E-15 -1.7973E-13 -3.8181E-12
 -4.1016E-13  5.9687E-13  8.9115E-15 -1.6653E-14  2.9687E-13  6.4662E-12
 -5.2444E-15  8.9115E-15  1.8542E-13 -9.2624E-14  4.3490E-15  1.0750E-13
  9.8460E-15 -1.6653E-14 -9.2624E-14  5.9527E-14 -9.3426E-15 -2.0011E-13
 -1.7973E-13  2.9687E-13  4.3490E-15 -9.3426E-15  2.7898E-13  3.4952E-12
 -3.8181E-12  6.4662E-12  1.0750E-13 -2.0011E-13  3.4952E-12  7.7786E-11
#      lat0       lon0       xBary       yBary       zBary        JD0
   -2.073434   49.145851   -0.094265   -0.035477   -0.984312  2456978.926868
# Heliocentric elements and errors
Epoch:              2456970.5000  =  2014/11/09
Mean Anomaly:          317.97559 +/-     0.038
Argument of Peri:      285.50390 +/-     0.070
Long of Asc Node:      181.62593 +/-     0.009
Inclination:             2.73673 +/-     0.000
Eccentricity:         0.17523247 +/-    0.0003
Semi-Major Axis:     46.00364533 +/-    0.0064
Time of Perihelion: 2470274.6139 +/-      11.6
Perihelion:          37.94231316 +/-    0.0154
Aphelion:            54.06497751 +/-    0.0163
Period (y)              312.0302 +/-      0.06
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           26.58786479 +/-    0.0005
Ecliptic Y           30.89278590 +/-    0.0006
Ecliptic Z           -1.44006185 +/-    0.0000
Ecliptic XDOT        -0.00238480 +/-    0.0000
Ecliptic YDOT         0.00154452 +/-    0.0000
Ecliptic ZDOT        -0.00007704 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   40.78421941 +/-    0.0006
Geocenter to KBO     39.80069759 +/-    0.0008
# Hcoef:  8.97

The following table shows the complete astrometric record for 15VV171. 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 (15VV171) followed by the observatory code and reference code for the source of the astrometry.

2014 11  17.42609  03 09 07.005  +15 30 51.24  24.6r 15VV171   568  C~2nwB      
2014 11  19.33914  03 08 57.467  +15 30 12.42  24.8r 15VV171   568  C~2nwB      
2014 11  23.44182  03 08 37.178  +15 28 50.45  25.0r 15VV171   568  C~2nwB      
2015 09  12.50083  03 19 28.694  +16 10 55.08  25.1w 15VV171   568  C~2nwB      
2015 10  08.43421  03 18 14.829  +16 04 54.95  25.3w 15VV171   568  C~2nwB      
2015 10  08.49327  03 18 14.616  +16 04 53.90  25.5w 15VV171   568  C~2nwB      
2015 11  07.34317  03 15 58.954  +15 55 17.85  24.8r 15VV171   568  C~2nwB      
2015 11  07.38533  03 15 58.730  +15 55 17.26  25.3r 15VV171   568  C~2nwB      
2015 11  07.42748  03 15 58.503  +15 55 16.27  24.9r 15VV171   568  C~2nwB      
2015 11  10.51130  03 15 42.966  +15 54 13.44  24.9w 15VV171   568  C~2nwB      
2015 11  17.35801  03 15 08.371  +15 51 55.13  25.3w 15VV171   568  C~2nwB      
2015 11  17.40462  03 15 08.118  +15 51 54.12  25.3w 15VV171   568  C~2nwB      
2015 12  06.36680  03 13 35.837  +15 45 57.71  25.3w 15VV171   568  C~2nwB      
2015 12  13.30120  03 13 05.223  +15 44 04.23  25.3w 15VV171   568  C~2nwB      
2015 12  13.35972  03 13 04.968  +15 44 03.24  25.5w 15VV171   568  C~2nwB      
2016 01  01.35451  03 11 56.314  +15 40 03.42  25.5w 15VV171   568  C~2nwB      
2016 02  04.33458  03 11 10.654  +15 38 29.65  26.5w 15VV171   568  C~2nwB      
2016 02  11.22361  03 11 15.435  +15 39 08.34  25.2w 15VV171   568  C~2nwB      
2016 09  07.56206  03 25 34.754  +16 31 18.63        15VV171   568  C~2nwB      
2016 09  26.62090  03 24 54.528  +16 27 47.15  25.5w 15VV171   568  C~2nwB      
2016 10  10.43747  03 24 06.862  +16 24 12.31  25.2w 15VV171   568  C~2nwB      
2016 10  10.49616  03 24 06.635  +16 24 11.34  25.1w 15VV171   568  C~2nwB      
2016 10  10.51394  03 24 06.570  +16 24 10.99  25.2w 15VV171   568  C~2nwB      
2016 11  02.51995  03 22 22.697  +16 17 00.97  25.4w 15VV171   568  C~2nwB      
2016 11  04.39506  03 22 13.383  +16 16 23.70  25.1w 15VV171   568  C~2nwB      
2016 12  24.33186  03 18 19.296  +16 01 56.35  25.1w 15VV171   568  C~2nwB      
2016 12  24.33677  03 18 19.270  +16 01 56.20  25.4w 15VV171   568  C~2nwB      
2016 12  28.44224  03 18 05.050  +16 01 09.50  25.5w 15VV171   568  C~2nwB      
2017 01  02.43457  03 17 49.567  +16 00 20.48  25.0w 15VV171   568  C~2nwB      
2017 01  02.43952  03 17 49.551  +16 00 20.40  25.0w 15VV171   568  C~2nwB      
2017 01  26.34976  03 17 06.202  +15 58 35.35  24.8w 15VV171   568  C~2nwB      
2017 09  15.58250  03 31 25.828  +16 49 21.55  25.4w 15VV171   568  C~2nwB      
2017 09  22.56874  03 31 10.749  +16 48 04.64  25.4w 15VV171   568  C~2nwB      
2017 12  13.39528  03 25 08.341  +16 24 33.31        15VV171   568  C~2nwB      
2017 12  13.43255  03 25 08.182  +16 24 32.50  25.1w 15VV171   568  C~2nwB      
2017 12  16.37785  03 24 55.408  +16 23 49.27  25.0w 15VV171   568  C~2nwB      

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     0.06
     2   0.0052   -143.22    -0.03      -0.14     0.06
     3   0.0165   -447.74    -0.08       0.25    -0.07
     4   0.8188   9293.38    -0.20     -51.05     0.11
     5   0.8898   8170.08    -0.17    -123.45     0.09
     6   0.8900   8166.83     0.07    -123.67    -0.02
     7   0.9717   6125.74     0.20    -169.43    -0.24
     8   0.9718   6122.47     0.14    -169.15     0.04
     9   0.9719   6119.05    -0.06    -169.24    -0.04
    10   0.9804   5886.09    -0.13    -171.07    -0.01
    11   0.9991   5367.79     0.05    -173.31    -0.01
    12   0.9993   5364.00    -0.16    -173.33    -0.04
    13   1.0512   3984.63     0.09    -165.37     0.00
    14   1.0702   3528.24    -0.04    -157.54     0.06
    15   1.0703   3524.43    -0.08    -157.52    -0.01
    16   1.1223   2504.75     0.12    -124.77    -0.03
    17   1.2154   1844.12     0.22     -38.85     0.12
    18   1.2342   1921.02     0.01     -20.06    -0.02
    19   1.8074  14718.69    -0.02    -209.22     0.00
    20   1.8595  14102.55     0.07    -268.64     0.13
    21   1.8974  13381.57    -0.04    -303.64     0.00
    22   1.8975  13378.15     0.09    -303.75    -0.01
    23   1.8976  13377.15     0.17    -303.85    -0.08
    24   1.9606  11816.03     0.12    -340.47     0.10
    25   1.9657  11676.40     0.04    -342.33    -0.03
    26   2.1024   8185.93     0.06    -312.79    -0.06
    27   2.1024   8185.53    -0.07    -312.84    -0.12
    28   2.1137   7975.11    -0.20    -304.70    -0.08
    29   2.1273   7746.47     0.09    -293.99    -0.09
    30   2.1273   7746.23     0.06    -294.01    -0.12
    31   2.1928   7114.55    -0.32    -232.54     0.18
    32   2.8286  19911.11     0.01    -408.90    -0.05
    33   2.8478  19680.27    -0.07    -430.74     0.17
    34   3.0718  14246.81    -0.09    -506.82     0.17
    35   3.0719  14244.38    -0.03    -507.03    -0.10
    36   3.0800  14054.72     0.11    -502.59    -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.

15VV171    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        46.334    46.349    46.319
ecceobj         0.175     0.176     0.175
incobj          2.727     2.727     2.727
qmin           36.976    36.921    37.010
qmax           55.466    55.395    55.351
amean          45.947    45.962    45.931
amin           45.548    45.564    45.535
amax           46.441    46.421    46.405
emean           0.177     0.178     0.176
emin            0.161     0.161     0.161
emax            0.194     0.194     0.193
imean           3.217     3.189     3.239
imin            2.306     2.191     2.412
imax            4.176     4.185     4.169
excite_mean     0.186     0.186     0.185
fracstop        1.000     1.000     1.000
cjmean          3.083     3.082     3.083

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       190.3     188.2     188.2
kozaiamp        179.9     179.9     180.0