Orbit Fit and Astrometric record for 15VH170

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: 15VH170   
# Created Tue Apr  1 01:10:41 2025
# Orbit generated from Bernstein formalism
# Fitting     35 observations of     35
# Arc:   2.09y
# First observation: 2015/08/20
#  Last observation: 2017/09/23
Preliminary a, adot, b, bdot, g, gdot:
  -0.000094   0.023468  -0.000002   0.000072   0.023710   0.000000
# Chi-squared of fit:     8.32 DOF:     64 RMS:  0.09
# Min/Max residuals:    -0.20    0.29
# Exact a, adot, b, bdot, g, gdot:
  1.503629E-05  2.308668E-02  7.911518E-07  6.973059E-05  2.346279E-02 -4.378784E-04
# Covariance matrix:
  2.1166E-13 -7.1532E-14  1.7391E-15 -3.8422E-16  1.2381E-13  1.6177E-12
 -7.1532E-14  3.0463E-13  1.8176E-15 -1.2674E-15  1.5150E-13  6.9989E-12
  1.7391E-15  1.8176E-15  1.2712E-13 -1.0409E-13  3.2612E-15  7.7199E-14
 -3.8422E-16 -1.2674E-15 -1.0409E-13  1.2546E-13 -1.2601E-15 -5.0183E-14
  1.2381E-13  1.5150E-13  3.2612E-15 -1.2601E-15  2.4595E-13  6.3417E-12
  1.6177E-12  6.9989E-12  7.7199E-14 -5.0183E-14  6.3417E-12  2.7491E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
   -1.299442   53.097676    1.012041   -0.001497   -0.071879  2457255.076589
# Heliocentric elements and errors
Epoch:              2457250.5000  =  2015/08/16
Mean Anomaly:          318.28799 +/-     0.394
Argument of Peri:      323.10078 +/-     0.475
Long of Asc Node:      135.54401 +/-     0.038
Inclination:             1.30452 +/-     0.000
Eccentricity:         0.06429763 +/-    0.0005
Semi-Major Axis:     44.76290752 +/-    0.0042
Time of Perihelion: 2469925.1067 +/-     119.6
Perihelion:          41.88475853 +/-    0.0242
Aphelion:            47.64105651 +/-    0.0243
Period (y)              299.4923 +/-      0.04
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           26.43352272 +/-    0.0005
Ecliptic Y           33.52297222 +/-    0.0007
Ecliptic Z           -0.96647933 +/-    0.0000
Ecliptic XDOT        -0.00218681 +/-    0.0000
Ecliptic YDOT         0.00157053 +/-    0.0000
Ecliptic ZDOT         0.00000935 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   42.70193055 +/-    0.0007
Geocenter to KBO     42.62067390 +/-    0.0009
# Hcoef:  8.39

The following table shows the complete astrometric record for 15VH170. 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 (15VH170) followed by the observatory code and reference code for the source of the astrometry.

2015 08  20.57580  03 24 10.870  +17 17 21.90  25.3w 15VH170   568  C~2nw5      
2015 09  07.61675  03 24 04.044  +17 16 23.57  24.8w 15VH170   568  C~2nw5      
2015 09  12.48448  03 23 57.091  +17 15 49.33  24.8w 15VH170   568  C~2nw5      
2015 10  09.56611  03 22 42.872  +17 10 33.67  25.1w 15VH170   568  C~2nw5      
2015 11  06.33360  03 20 41.380  +17 02 37.30  24.8r 15VH170   568  C~2nw5      
2015 11  06.39716  03 20 41.088  +17 02 36.21  24.1r 15VH170   568  C~2nw5      
2015 11  06.40423  03 20 41.031  +17 02 36.04  24.2r 15VH170   568  C~2nw5      
2015 11  06.47375  03 20 40.714  +17 02 34.98  24.6r 15VH170   568  C~2nw5      
2015 11  07.49015  03 20 35.769  +17 02 15.99  24.8w 15VH170   568  C~2nw5      
2015 11  17.47779  03 19 46.961  +16 59 10.61  24.8w 15VH170   568  C~2nw5      
2015 12  06.33759  03 18 17.522  +16 53 38.65  25.0w 15VH170   568  C~2nw5      
2015 12  06.47504  03 18 16.921  +16 53 36.49  24.3w 15VH170   568  C~2nw5      
2016 01  07.39390  03 16 22.632  +16 46 57.34  25.1w 15VH170   568  C~2nw5      
2016 02  04.37827  03 15 49.883  +16 45 43.08  25.0w 15VH170   568  C~2nw5      
2016 02  11.24684  03 15 53.369  +16 46 10.32  25.0w 15VH170   568  C~2nw5      
2016 09  07.57941  03 29 27.510  +17 36 16.41        15VH170   568  C~2nw5      
2016 09  07.59099  03 29 27.494  +17 36 16.33        15VH170   568  C~2nw5      
2016 09  27.51468  03 28 47.034  +17 33 18.77  24.7w 15VH170   568  C~2nw5      
2016 09  29.49059  03 28 41.249  +17 32 55.02  25.0w 15VH170   568  C~2nw5      
2016 10  07.49825  03 28 14.874  +17 31 09.77  24.4w 15VH170   568  C~2nw5      
2016 10  07.50982  03 28 14.832  +17 31 09.35  24.9w 15VH170   568  C~2nw5      
2016 10  07.59395  03 28 14.521  +17 31 08.29  24.6w 15VH170   568  C~2nw5      
2016 10  07.60551  03 28 14.485  +17 31 08.13  24.6w 15VH170   568  C~2nw5      
2016 10  09.49835  03 28 07.612  +17 30 40.99  25.6w 15VH170   568  C~2nw5      
2016 10  09.51019  03 28 07.570  +17 30 40.90  24.8w 15VH170   568  C~2nw5      
2016 10  09.57103  03 28 07.336  +17 30 39.93  25.2w 15VH170   568  C~2nw5      
2016 10  09.58259  03 28 07.295  +17 30 39.88  25.6w 15VH170   568  C~2nw5      
2016 11  02.49681  03 26 24.303  +17 24 07.03  25.2w 15VH170   568  C~2nw5      
2016 11  04.47292  03 26 14.852  +17 23 31.72  24.8w 15VH170   568  C~2nw5      
2016 12  28.46047  03 22 13.311  +17 09 11.52  25.0w 15VH170   568  C~2nw5      
2016 12  29.39076  03 22 10.308  +17 09 01.52  25.3w 15VH170   568  C~2nw5      
2017 01  27.29772  03 21 12.397  +17 06 14.88  24.8w 15VH170   568  C~2nw5      
2017 01  27.30287  03 21 12.400  +17 06 14.83  24.9w 15VH170   568  C~2nw5      
2017 09  16.62789  03 34 40.518  +17 54 42.15  24.8w 15VH170   568  C~2nw5      
2017 09  23.56691  03 34 25.711  +17 53 39.64  25.1w 15VH170   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     0.11       0.00    -0.15
     2   0.0494   -109.25     0.01     -32.01    -0.03
     3   0.0627   -214.25    -0.07     -40.23     0.01
     4   0.1369  -1322.85    -0.08     -78.63    -0.04
     5   0.2129  -3128.65    -0.08     -98.40    -0.03
     6   0.2131  -3132.98     0.21     -98.38    -0.03
     7   0.2131  -3133.82    -0.11     -98.34     0.01
     8   0.2133  -3138.48     0.29     -98.21     0.14
     9   0.2161  -3211.92    -0.11     -98.52     0.07
    10   0.2434  -3936.35    -0.04     -99.16    -0.03
    11   0.2950  -5262.60    -0.20     -90.78     0.09
    12   0.2954  -5271.49     0.18     -90.65     0.09
    13   0.3828  -6961.23    -0.17     -51.84    -0.01
    14   0.4594  -7435.27     0.06      -1.16     0.02
    15   0.4782  -7379.76     0.05      12.11    -0.02
    16   1.0513   4671.71    -0.01     -18.94    -0.03
    17   1.0514   4671.47    -0.04     -18.96    -0.04
    18   1.1059   4066.81    -0.00     -50.06    -0.01
    19   1.1113   3980.74     0.01     -52.87    -0.12
    20   1.1333   3589.08     0.02     -62.60     0.12
    21   1.1333   3588.40    -0.04     -62.86    -0.13
    22   1.1335   3583.82    -0.06     -62.80     0.01
    23   1.1336   3583.28     0.03     -62.83    -0.01
    24   1.1387   3481.29    -0.00     -65.04    -0.07
    25   1.1388   3480.68     0.06     -64.98    -0.01
    26   1.1389   3477.20    -0.02     -65.10    -0.07
    27   1.1390   3476.62     0.05     -65.01     0.03
    28   1.2044   1951.26    -0.09     -82.84     0.06
    29   1.2098   1811.43     0.00     -83.57    -0.00
    30   1.3577  -1753.56    -0.12     -51.24     0.17
    31   1.3602  -1797.73     0.08     -50.04     0.05
    32   1.4393  -2643.11    -0.00      -1.00     0.02
    33   1.4394  -2643.08     0.08      -1.06    -0.05
    34   2.0754   9283.26    -0.01     -19.13     0.04
    35   2.0944   9062.68     0.03     -29.81    -0.04

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.

15VH170    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        45.191    45.201    45.181
ecceobj         0.067     0.068     0.067
incobj          1.304     1.304     1.304
qmin           40.989    40.979    40.975
qmax           48.933    48.965    48.889
amean          44.833    44.842    44.823
amin           44.482    44.495    44.460
amax           45.205    45.224    45.191
emean           0.068     0.068     0.067
emin            0.054     0.055     0.053
emax            0.083     0.083     0.082
imean           1.218     1.216     1.219
imin            0.595     0.595     0.596
imax            1.722     1.720     1.724
excite_mean     0.071     0.072     0.071
fracstop        1.000     1.000     1.000
cjmean          3.105     3.106     3.105

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       197.2     197.3     197.1
kozaiamp        180.0     179.9     180.0