Orbit Fit and Astrometric record for 15VE171

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: 15VE171   
# Created Sat Apr 27 01:17:51 2024
# Orbit generated from Bernstein formalism
# Fitting     35 observations of     36
# Arc:   2.27y
# First observation: 2015/09/07
#  Last observation: 2017/12/16
Preliminary a, adot, b, bdot, g, gdot:
  -0.000074   0.019177  -0.000002   0.000531   0.021544   0.000000
# Chi-squared of fit:     5.48 DOF:     64 RMS:  0.07
# Min/Max residuals:    -0.18    0.18
# Exact a, adot, b, bdot, g, gdot:
  1.421844E-05  1.902666E-02  2.151173E-07  5.265189E-04  2.148975E-02 -7.339607E-04
# Covariance matrix:
  1.9991E-13 -2.0742E-15  5.1670E-17  2.6325E-15  1.4593E-13  2.5380E-12
 -2.0742E-15  2.5117E-13 -1.2847E-15  7.8033E-15  1.5860E-13  7.3996E-12
  5.1670E-17 -1.2847E-15  9.4180E-14 -5.9117E-14 -6.0828E-16 -5.0028E-14
  2.6325E-15  7.8033E-15 -5.9117E-14  6.6367E-14  6.9385E-15  3.1257E-13
  1.4593E-13  1.5860E-13 -6.0828E-16  6.9385E-15  2.4277E-13  6.6254E-12
  2.5380E-12  7.3996E-12 -5.0028E-14  3.1257E-13  6.6254E-12  2.9652E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.942123   51.732615    0.931848   -0.006301   -0.392225  2457273.133899
# Heliocentric elements and errors
Epoch:              2457270.5000  =  2015/09/05
Mean Anomaly:          225.37252 +/-     0.410
Argument of Peri:      110.69855 +/-     0.405
Long of Asc Node:       81.35758 +/-     0.012
Inclination:             1.82599 +/-     0.001
Eccentricity:         0.09094379 +/-    0.0005
Semi-Major Axis:     43.95710038 +/-    0.0047
Time of Perihelion: 2497078.7613 +/-     121.1
Perihelion:          39.95947529 +/-    0.0244
Aphelion:            47.95472548 +/-    0.0245
Period (y)              291.4417 +/-      0.05
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           29.78646608 +/-    0.0007
Ecliptic Y           36.26074526 +/-    0.0008
Ecliptic Z           -0.76511072 +/-    0.0000
Ecliptic XDOT        -0.00196228 +/-    0.0000
Ecliptic YDOT         0.00142233 +/-    0.0000
Ecliptic ZDOT         0.00006866 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   46.93251115 +/-    0.0008
Geocenter to KBO     46.53380807 +/-    0.0011
# Hcoef:  8.00

The following table shows the complete astrometric record for 15VE171. 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 (15VE171) followed by the observatory code and reference code for the source of the astrometry.

2015 09  07.63311  03 18 16.256  +17 17 17.59  25.2w 15VE171   568  C~2nw8      
2015 09  12.49674  03 18 08.982  +17 16 45.53  24.4w 15VE171   568  C~2nw8      
2015 10  07.54436  03 17 03.778  +17 12 18.57  25.0w 15VE171   568  C~2nw8      
2015 10  07.60373  03 17 03.574  +17 12 17.72  25.1w 15VE171   568  C~2nw8      
2015 10  09.58362  03 16 56.691  +17 11 50.20  25.1w 15VE171   568  C~2nw8      
2015 11  07.33788  03 14 58.418  +17 04 07.69  24.6r 15VE171   568  C~2nw8      
2015 11  07.38006  03 14 58.234  +17 04 07.02  24.8r 15VE171   568  C~2nw8      
2015 11  07.42224  03 14 58.050  +17 04 06.18  24.6r 15VE171   568  C~2nw8      
2015 11  10.50536  03 14 44.123  +17 03 12.72  25.0w 15VE171   568  C~2nw8      
2015 11  17.35218  03 14 13.174  +17 01 13.80  25.0w 15VE171   568  C~2nw8      
2015 11  17.39878  03 14 12.957  +17 01 13.01  24.7w 15VE171   568  C~2nw8      
2015 12  06.36096  03 12 50.370  +16 56 00.38  24.6w 15VE171   568  C~2nw8      
2015 12  06.49848  03 12 49.821  +16 55 58.49  25.0w 15VE171   568  C~2nw8      
2016 01  01.34872  03 11 20.663  +16 50 33.61  24.8w 15VE171   568  C~2nw8      
2016 01  07.41130  03 11 05.913  +16 49 43.14  24.4w 15VE171   568  C~2nw8      
2016 01  07.42868  03 11 05.861  +16 49 42.94  24.1w 15VE171   568  C~2nw8      
2016 01  08.25624  03 11 04.092  +16 49 37.01  25.0w 15VE171   568  C~2nw8      
2016 02  05.28768  03 10 37.083  +16 48 31.84  25.1w 15VE171   568  C~2nw8      
2016 02  10.30807  03 10 39.545  +16 48 49.65  25.0w 15VE171   568  C~2nw8      
2016 09  07.62568  03 22 38.378  +17 35 39.54        15VE171   568  C~2nw8      
2016 09  26.58416  03 22 00.040  +17 33 02.32  24.8w 15VE171   568  C~2nw8      
2016 10  09.54522  03 21 19.322  +17 30 22.85  25.3w 15VE171   568  C~2nw8      
2016 10  09.61729  03 21 19.070  +17 30 21.92  25.1w 15VE171   568  C~2nw8      
2016 11  02.52573  03 19 42.200  +17 24 11.96  24.7w 15VE171   568  C~2nw8      
2016 11  04.40084  03 19 33.857  +17 23 40.49  24.8w 15VE171   568  C~2nw8      
2016 12  24.31334  03 16 05.146  +17 10 53.36  24.9w 15VE171   568  C~2nw8      
2017 01  02.41556  03 15 38.478  +17 09 21.15  25.2w 15VE171   568  C~2nw8      
2017 01  26.32908  03 14 58.685  +17 07 20.45  24.7w 15VE171   568  C~2nw8      
2017 09  15.58856  03 26 50.975  +17 52 56.88  25.3w 15VE171   568  C~2nw8      
2017 09  17.60038  03 26 47.162  +17 52 41.54  25.2w 15VE171   568  C~2nw8      
2017 09  22.57478  03 26 36.377  +17 51 59.01  24.9w 15VE171   568  C~2nw8      
2017 09  23.57901  03 26 33.975  +17 51 49.78  25.2w 15VE171   568  C~2nw8      
2017 09  24.59522  03 26 31.456  +17 51 39.90  25.0w 15VE171   568  C~2nw8      
2017 12  16.34929  03 20 58.947  +17 31 19.81  24.9w 15VE171   568  C~2nw8      
2017 12  16.36856  03 20 58.869  +17 31 19.61  24.7w 15VE171   568  C~2nw8      
2017 12  16.39181  03 20 58.779  +17 31 19.22  25.3w 15VE171   568  C~2nw8      

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     0.04
     2   0.0133   -108.93     0.02      -4.09    -0.02
     3   0.0819  -1080.31    -0.05     -20.16     0.09
     4   0.0821  -1083.35    -0.01     -20.22     0.05
     5   0.0875  -1185.75    -0.05     -21.20    -0.04
     6   0.1662  -2943.25    -0.07     -25.38     0.09
     7   0.1663  -2945.97     0.06     -25.33     0.11
     8   0.1664  -2948.74     0.15     -25.45    -0.03
     9   0.1749  -3155.53    -0.18     -24.66     0.14
    10   0.1936  -3615.16     0.01     -22.79    -0.03
    11   0.1937  -3618.37    -0.02     -22.73    -0.01
    12   0.2457  -4844.22     0.15     -11.61    -0.06
    13   0.2460  -4852.32 (   0.55)    -11.34 (   0.08)
    14   0.3168  -6173.29    -0.03      15.43     0.01
    15   0.3334  -6391.04     0.04      23.28    -0.00
    16   0.3335  -6391.82    -0.16      23.28    -0.02
    17   0.3357  -6417.90     0.08      24.35    -0.04
    18   0.4125  -6809.43    -0.04      65.18    -0.11
    19   0.4262  -6770.56     0.10      72.90    -0.06
    20   1.0020   3908.54     0.05     107.96    -0.01
    21   1.0539   3338.19    -0.04      94.49    -0.07
    22   1.0894   2734.25    -0.02      88.02    -0.10
    23   1.0896   2730.52     0.10      88.03    -0.06
    24   1.1551   1295.72     0.07      84.05    -0.03
    25   1.1602   1172.22     0.03      84.24     0.01
    26   1.2969  -1913.77    -0.02     116.13     0.03
    27   1.3218  -2306.83     0.03     126.87    -0.01
    28   1.3873  -2889.02    -0.08     159.66    -0.02
    29   2.0231   7665.13    -0.03     211.07    -0.00
    30   2.0287   7608.52     0.05     209.65    -0.05
    31   2.0423   7448.60     0.01     206.51     0.03
    32   2.0450   7413.04     0.06     206.05     0.18
    33   2.0478   7375.70    -0.13     205.37     0.11
    34   2.2744   2466.82     0.03     217.25    -0.05
    35   2.2744   2465.69    -0.01     217.34     0.02
    36   2.2745   2464.35    -0.04     217.29    -0.06

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.

15VE171    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        44.334    44.345    44.323
ecceobj         0.081     0.082     0.080
incobj          1.824     1.824     1.824
qmin           39.368    39.325    39.402
qmax           48.986    49.024    48.913
amean          44.045    44.057    44.033
amin           43.688    43.704    43.691
amax           44.424    44.445    44.404
emean           0.085     0.087     0.084
emin            0.069     0.070     0.068
emax            0.103     0.104     0.102
imean           0.734     0.735     0.732
imin            0.355     0.351     0.357
imax            1.118     1.124     1.107
excite_mean     0.086     0.088     0.085
fracstop        1.000     1.000     1.000
cjmean          3.093     3.093     3.093

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       180.5     181.9     179.8
kozaiamp        180.0     180.0     179.9