Orbit Fit and Astrometric record for 15VE172

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: 15VE172   
# Created Tue Apr  1 01:10:42 2025
# Orbit generated from Bernstein formalism
# Fitting     35 observations of     35
# Arc:   2.35y
# First observation: 2015/08/11
#  Last observation: 2017/12/16
Preliminary a, adot, b, bdot, g, gdot:
  -0.000095   0.020383  -0.000007   0.000780   0.022241   0.000000
# Chi-squared of fit:     6.22 DOF:     64 RMS:  0.07
# Min/Max residuals:    -0.17    0.19
# Exact a, adot, b, bdot, g, gdot:
  1.487551E-05  2.007238E-02  8.549498E-07  7.676481E-04  2.199936E-02  1.581295E-03
# Covariance matrix:
  1.8898E-13 -2.1240E-14  4.3045E-15  1.4157E-15  1.2773E-13  1.7821E-12
 -2.1240E-14  2.8065E-13  2.9486E-15  6.4700E-15  1.6979E-13  7.8292E-12
  4.3045E-15  2.9486E-15  9.7009E-14 -6.6661E-14  6.4559E-15  1.1522E-13
  1.4157E-15  6.4700E-15 -6.6661E-14  7.9600E-14  5.4065E-15  2.5169E-13
  1.2773E-13  1.6979E-13  6.4559E-15  5.4065E-15  2.4069E-13  6.6176E-12
  1.7821E-12  7.8292E-12  1.1522E-13  2.5169E-13  6.6176E-12  3.0457E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
   -3.029563   51.570705    1.014477    0.002951    0.053395  2457246.102289
# Heliocentric elements and errors
Epoch:              2457240.5000  =  2015/08/06
Mean Anomaly:          121.54275 +/-     0.476
Argument of Peri:      177.19211 +/-     0.467
Long of Asc Node:      105.36882 +/-     0.010
Inclination:             3.69684 +/-     0.000
Eccentricity:         0.06542618 +/-    0.0006
Semi-Major Axis:     43.78270013 +/-    0.0050
Time of Perihelion: 2421514.9599 +/-     139.7
Perihelion:          40.91816517 +/-    0.0284
Aphelion:            46.64723510 +/-    0.0286
Period (y)              289.7090 +/-      0.05
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           28.97097040 +/-    0.0006
Ecliptic Y           34.88678750 +/-    0.0008
Ecliptic Z           -2.40232967 +/-    0.0001
Ecliptic XDOT        -0.00183367 +/-    0.0000
Ecliptic YDOT         0.00170420 +/-    0.0000
Ecliptic ZDOT         0.00008506 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   45.41119087 +/-    0.0007
Geocenter to KBO     45.45587706 +/-    0.0010
# Hcoef:  8.33

The following table shows the complete astrometric record for 15VE172. 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 (15VE172) followed by the observatory code and reference code for the source of the astrometry.

2015 08  11.60150  03 19 51.338  +15 13 45.65  25.7w 15VE172   568  C~2nwC      
2015 09  06.61481  03 19 49.349  +15 12 01.75  25.3w 15VE172   568  C~2nwC      
2015 09  12.50491  03 19 40.891  +15 11 08.88  25.0w 15VE172   568  C~2nwC      
2015 10  07.42821  03 18 35.752  +15 05 47.39  25.4w 15VE172   568  C~2nwC      
2015 10  08.44001  03 18 32.230  +15 05 31.56  25.0w 15VE172   568  C~2nwC      
2015 10  08.49908  03 18 32.019  +15 05 30.77  25.1w 15VE172   568  C~2nwC      
2015 11  07.34843  03 16 28.051  +14 56 55.66  24.6r 15VE172   568  C~2nwC      
2015 11  07.39058  03 16 27.858  +14 56 54.98  25.1r 15VE172   568  C~2nwC      
2015 11  07.43274  03 16 27.660  +14 56 54.09  24.8r 15VE172   568  C~2nwC      
2015 11  10.51713  03 16 13.515  +14 55 59.05  25.2w 15VE172   568  C~2nwC      
2015 11  17.36382  03 15 41.961  +14 53 59.02  24.9w 15VE172   568  C~2nwC      
2015 11  17.41043  03 15 41.741  +14 53 58.28  24.9w 15VE172   568  C~2nwC      
2015 12  06.37266  03 14 17.493  +14 48 55.29  24.6w 15VE172   568  C~2nwC      
2015 12  13.30706  03 13 49.459  +14 47 21.60  24.8w 15VE172   568  C~2nwC      
2015 12  13.36559  03 13 49.230  +14 47 20.72  24.8w 15VE172   568  C~2nwC      
2016 01  01.36029  03 12 45.836  +14 44 11.79  24.9w 15VE172   568  C~2nwC      
2016 01  07.30705  03 12 31.014  +14 43 36.29  25.5w 15VE172   568  C~2nwC      
2016 02  04.34036  03 12 00.889  +14 43 42.69  25.5w 15VE172   568  C~2nwC      
2016 02  11.22942  03 12 04.262  +14 44 28.69  25.4w 15VE172   568  C~2nwC      
2016 09  07.56785  03 24 23.272  +15 31 59.82        15VE172   568  C~2nwC      
2016 09  25.60501  03 23 47.684  +15 28 49.96  25.0w 15VE172   568  C~2nwC      
2016 10  10.44325  03 23 00.838  +15 25 18.58  25.1w 15VE172   568  C~2nwC      
2016 10  10.50202  03 23 00.626  +15 25 17.64  25.4w 15VE172   568  C~2nwC      
2016 10  10.51973  03 23 00.557  +15 25 17.33  25.4w 15VE172   568  C~2nwC      
2016 10  10.53987  03 23 00.480  +15 25 16.97  25.5w 15VE172   568  C~2nwC      
2016 11  02.51417  03 21 25.780  +15 18 51.25  24.7w 15VE172   568  C~2nwC      
2016 11  04.38927  03 21 17.316  +15 18 18.47  24.7w 15VE172   568  C~2nwC      
2016 12  24.31885  03 17 44.698  +15 06 04.20  25.3w 15VE172   568  C~2nwC      
2017 01  02.42106  03 17 17.419  +15 04 51.09  25.3w 15VE172   568  C~2nwC      
2017 01  26.33541  03 16 36.546  +15 03 54.22  25.0w 15VE172   568  C~2nwC      
2017 09  16.63393  03 28 45.815  +15 50 29.00  25.0w 15VE172   568  C~2nwC      
2017 09  17.59434  03 28 43.986  +15 50 19.17  24.9w 15VE172   568  C~2nwC      
2017 09  23.57295  03 28 30.860  +15 49 13.84  25.1w 15VE172   568  C~2nwC      
2017 12  16.34460  03 22 51.754  +15 28 00.12  25.2w 15VE172   568  C~2nwC      
2017 12  16.35926  03 22 51.696  +15 27 59.86  25.2w 15VE172   568  C~2nwC      

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    -0.09       0.00    -0.06
     2   0.0712    -54.45    -0.08     -93.05     0.08
     3   0.0873   -186.35     0.16    -112.77    -0.02
     4   0.1556  -1180.47    -0.01    -181.04    -0.04
     5   0.1584  -1233.84    -0.05    -183.19    -0.08
     6   0.1585  -1237.00    -0.00    -183.17     0.05
     7   0.2402  -3105.33     0.04    -215.89     0.01
     8   0.2404  -3108.21     0.10    -215.82     0.07
     9   0.2405  -3111.21     0.03    -215.93    -0.06
    10   0.2489  -3323.52     0.18    -215.76    -0.17
    11   0.2677  -3796.50    -0.02    -212.51    -0.03
    12   0.2678  -3799.77    -0.03    -212.39     0.04
    13   0.3197  -5058.56    -0.11    -185.36     0.04
    14   0.3387  -5475.72    -0.09    -169.01     0.11
    15   0.3388  -5479.16    -0.08    -168.99    -0.04
    16   0.3909  -6416.75    -0.11    -109.04     0.04
    17   0.4071  -6633.73     0.07     -86.48    -0.01
    18   0.4839  -7053.96     0.17      35.35     0.19
    19   0.5027  -6994.53    -0.04      66.77     0.02
    20   1.0759   4082.35    -0.01      60.56     0.04
    21   1.1253   3536.56     0.06       6.16    -0.12
    22   1.1659   2827.68    -0.03     -27.52     0.05
    23   1.1661   2824.47     0.03     -27.65     0.00
    24   1.1661   2823.43    -0.03     -27.70    -0.02
    25   1.1662   2822.26    -0.07     -27.77    -0.05
    26   1.2291   1399.36     0.03     -53.51     0.01
    27   1.2342   1272.59     0.02     -54.04     0.01
    28   1.3709  -1890.50     0.04      26.03    -0.05
    29   1.3958  -2291.07    -0.04      57.67    -0.08
    30   1.4613  -2877.65    -0.08     156.34     0.04
    31   2.1000   8034.05    -0.05     192.18     0.06
    32   2.1026   8006.00     0.09     189.15    -0.13
    33   2.1190   7806.03    -0.10     172.47     0.10
    34   2.3484   2741.42     0.06     161.99     0.05
    35   2.3484   2740.55     0.03     161.95    -0.03

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.

15VE172    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        44.199    44.217    44.182
ecceobj         0.065     0.067     0.063
incobj          3.698     3.698     3.698
qmin           40.384    40.308    40.424
qmax           47.632    47.663    47.515
amean          43.882    43.898    43.866
amin           43.539    43.546    43.521
amax           44.253    44.260    44.238
emean           0.060     0.062     0.058
emin            0.043     0.045     0.041
emax            0.077     0.078     0.075
imean           2.078     2.077     2.080
imin            1.343     1.342     1.344
imax            2.726     2.723     2.727
excite_mean     0.071     0.072     0.069
fracstop        1.000     1.000     1.000
cjmean          3.094     3.094     3.094

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       180.9     181.1     181.1
kozaiamp        180.0     180.0     180.0