Orbit Fit and Astrometric record for 15VJ170

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: 15VJ170   
# Created Tue Apr  1 01:10:41 2025
# Orbit generated from Bernstein formalism
# Fitting     34 observations of     34
# Arc:   2.27y
# First observation: 2015/09/07
#  Last observation: 2017/12/13
Preliminary a, adot, b, bdot, g, gdot:
  -0.000089   0.020978  -0.000003   0.001620   0.022681   0.000000
# Chi-squared of fit:     5.65 DOF:     62 RMS:  0.07
# Min/Max residuals:    -0.18    0.16
# Exact a, adot, b, bdot, g, gdot:
  1.473517E-05  2.080929E-02  1.008319E-06  1.608618E-03  2.262657E-02  1.318477E-04
# Covariance matrix:
  1.8963E-13 -4.6495E-14  3.2914E-16  4.2610E-15  1.2545E-13  1.5184E-12
 -4.6495E-14  2.9054E-13 -4.2709E-15  2.2024E-14  1.4341E-13  7.4895E-12
  3.2914E-16 -4.2709E-15  1.0146E-13 -7.5979E-14 -1.9631E-15 -1.6063E-13
  4.2610E-15  2.2024E-14 -7.5979E-14  9.9444E-14  1.7503E-14  8.5649E-13
  1.2545E-13  1.4341E-13 -1.9631E-15  1.7503E-14  2.3500E-13  6.0382E-12
  1.5184E-12  7.4895E-12 -1.6063E-13  8.5649E-13  6.0382E-12  2.9158E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
   -1.867743   52.512004    0.937182   -0.012216   -0.379174  2457273.121609
# Heliocentric elements and errors
Epoch:              2457270.5000  =  2015/09/05
Mean Anomaly:          203.52200 +/-     0.930
Argument of Peri:      135.46976 +/-     0.930
Long of Asc Node:       74.16792 +/-     0.004
Inclination:             4.75724 +/-     0.001
Eccentricity:         0.04431532 +/-    0.0003
Semi-Major Axis:     42.82932349 +/-    0.0028
Time of Perihelion: 2501770.6047 +/-     264.4
Perihelion:          40.93132838 +/-    0.0139
Aphelion:            44.72731859 +/-    0.0140
Period (y)              280.2980 +/-      0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           27.85351212 +/-    0.0006
Ecliptic Y           34.78034205 +/-    0.0007
Ecliptic Z           -1.44039954 +/-    0.0000
Ecliptic XDOT        -0.00198625 +/-    0.0000
Ecliptic YDOT         0.00154368 +/-    0.0000
Ecliptic ZDOT         0.00019408 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   44.58211616 +/-    0.0007
Geocenter to KBO     44.19583563 +/-    0.0009
# Hcoef:  8.02

The following table shows the complete astrometric record for 15VJ170. 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 (15VJ170) followed by the observatory code and reference code for the source of the astrometry.

2015 09  07.62082  03 22 24.546  +16 35 31.91  24.9w 15VJ170   568  C~2nw5      
2015 09  12.48448  03 22 17.422  +16 34 57.83  24.8w 15VJ170   568  C~2nw5      
2015 10  07.52687  03 21 11.251  +16 30 20.42  24.6w 15VJ170   568  C~2nw5      
2015 10  07.58621  03 21 11.041  +16 30 19.69  24.6w 15VJ170   568  C~2nw5      
2015 10  09.56611  03 21 03.958  +16 29 51.53  24.8w 15VJ170   568  C~2nw5      
2015 11  06.33883  03 19 05.787  +16 22 20.02  24.2r 15VJ170   568  C~2nw5      
2015 11  06.40946  03 19 05.455  +16 22 19.12  24.2r 15VJ170   568  C~2nw5      
2015 11  06.47899  03 19 05.119  +16 22 17.71  24.3r 15VJ170   568  C~2nw5      
2015 11  07.49597  03 19 00.348  +16 22 00.09  24.3w 15VJ170   568  C~2nw5      
2015 11  17.47779  03 18 13.147  +16 19 07.72  24.6w 15VJ170   568  C~2nw5      
2015 11  17.56554  03 18 12.722  +16 19 06.11  24.7w 15VJ170   568  C~2nw5      
2015 12  06.34344  03 16 46.722  +16 14 03.75  24.8w 15VJ170   568  C~2nw5      
2015 12  06.48092  03 16 46.110  +16 14 01.74  24.4w 15VJ170   568  C~2nw5      
2015 12  31.36453  03 15 14.282  +16 09 07.38  24.6w 15VJ170   568  C~2nw5      
2016 01  07.39390  03 14 55.678  +16 08 16.31  24.7w 15VJ170   568  C~2nw5      
2016 02  05.29346  03 14 23.508  +16 07 49.28  24.7w 15VJ170   568  C~2nw5      
2016 02  11.24684  03 14 26.436  +16 08 21.87  24.8w 15VJ170   568  C~2nw5      
2016 09  07.57941  03 27 06.939  +16 58 39.20  24.8w 15VJ170   568  C~2nw5      
2016 09  27.51468  03 26 26.038  +16 55 45.63  24.8w 15VJ170   568  C~2nw5      
2016 09  29.49059  03 26 20.292  +16 55 22.73  25.0w 15VJ170   568  C~2nw5      
2016 10  05.49370  03 26 01.197  +16 54 07.89  24.8w 15VJ170   568  C~2nw5      
2016 10  07.49825  03 25 54.310  +16 53 41.33  24.8w 15VJ170   568  C~2nw5      
2016 10  07.59395  03 25 53.970  +16 53 39.96  24.9w 15VJ170   568  C~2nw5      
2016 10  09.49835  03 25 47.178  +16 53 13.74  24.9w 15VJ170   568  C~2nw5      
2016 10  09.57103  03 25 46.912  +16 53 12.76  24.8w 15VJ170   568  C~2nw5      
2016 11  02.48525  03 24 06.602  +16 46 59.78  24.8w 15VJ170   568  C~2nw5      
2016 11  04.46126  03 23 57.431  +16 46 26.55  24.6w 15VJ170   568  C~2nw5      
2016 12  28.46047  03 20 04.312  +16 33 22.75  25.0w 15VJ170   568  C~2nw5      
2016 12  29.39076  03 20 01.402  +16 33 14.22  24.9w 15VJ170   568  C~2nw5      
2017 01  27.30287  03 19 05.441  +16 31 12.10  24.7w 15VJ170   568  C~2nw5      
2017 09  15.58250  03 31 39.839  +17 20 35.85        15VJ170   568  C~2nw5      
2017 09  21.62755  03 31 27.494  +17 19 45.40  24.9w 15VJ170   568  C~2nw5      
2017 09  22.56874  03 31 25.305  +17 19 36.67  24.8w 15VJ170   568  C~2nw5      
2017 12  13.43255  03 25 46.035  +16 59 48.93        15VJ170   568  C~2nw5      

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    -0.04       0.00     0.02
     2   0.0133   -107.70     0.06      -7.10    -0.02
     3   0.0819  -1098.43    -0.03     -34.34    -0.04
     4   0.0820  -1101.53     0.04     -34.28     0.05
     5   0.0875  -1207.22    -0.02     -35.62     0.04
     6   0.1635  -2966.48    -0.01     -37.95    -0.16
     7   0.1637  -2971.33     0.12     -37.60     0.13
     8   0.1639  -2976.37    -0.00     -37.72    -0.05
     9   0.1667  -3047.27    -0.04     -37.13    -0.03
    10   0.1940  -3748.34     0.05     -29.00    -0.09
    11   0.1942  -3754.67    -0.03     -28.98    -0.16
    12   0.2456  -5029.62     0.04      -1.00    -0.10
    13   0.2460  -5038.66    -0.04      -0.65    -0.04
    14   0.3142  -6393.51    -0.07      59.38     0.11
    15   0.3334  -6665.87     0.08      80.14     0.16
    16   0.4125  -7120.83    -0.08     175.47     0.15
    17   0.4288  -7071.52    -0.02     195.87     0.01
    18   1.0019   4273.99     0.01     330.56    -0.01
    19   1.0565   3662.21     0.05     307.48     0.01
    20   1.0619   3576.63    -0.12     305.72     0.01
    21   1.0784   3292.51    -0.18     301.18     0.06
    22   1.0839   3190.14     0.03     299.99     0.15
    23   1.0841   3185.07     0.06     299.88     0.07
    24   1.0893   3084.11    -0.05     298.70    -0.00
    25   1.0895   3080.16     0.01     298.70     0.02
    26   1.1550   1592.29     0.08     296.85    -0.01
    27   1.1604   1456.45     0.03     297.69    -0.07
    28   1.3083  -1982.86     0.05     387.20    -0.01
    29   1.3108  -2025.49    -0.00     389.64    -0.08
    30   1.3900  -2834.75     0.03     477.64    -0.09
    31   2.0232   8392.34    -0.04     653.24    -0.01
    32   2.0397   8208.32     0.08     646.92    -0.06
    33   2.0423   8175.75     0.02     646.01    -0.05
    34   2.2664   3166.45    -0.05     685.61     0.09

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.

15VJ170    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        43.213    43.222    43.204
ecceobj         0.034     0.034     0.035
incobj          4.747     4.747     4.747
qmin           40.445    40.425    40.352
qmax           45.564    45.596    45.666
amean          42.917    42.925    42.908
amin           42.585    42.591    42.575
amax           43.259    43.261    43.252
emean           0.035     0.034     0.035
emin            0.017     0.016     0.016
emax            0.054     0.054     0.056
imean           2.775     2.779     2.771
imin            1.884     1.891     1.877
imax            3.773     3.770     3.775
excite_mean     0.060     0.059     0.060
fracstop        1.000     1.000     1.000
cjmean          3.085     3.085     3.084

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       182.3     182.2     182.7
kozaiamp        180.0     180.0     179.9