Orbit Fit and Astrometric record for 15VQ170

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: 15VQ170   
# Created Tue Apr  1 01:10:41 2025
# Orbit generated from Bernstein formalism
# Fitting     35 observations of     35
# Arc:   2.20y
# First observation: 2014/11/17
#  Last observation: 2017/01/27
Preliminary a, adot, b, bdot, g, gdot:
  -0.000038   0.028769   0.000000   0.005358   0.027265   0.000000
# Chi-squared of fit:     5.98 DOF:     64 RMS:  0.07
# Min/Max residuals:    -0.16    0.23
# Exact a, adot, b, bdot, g, gdot:
  1.700402E-05  2.880802E-02  3.212792E-06  5.375894E-03  2.723227E-02 -2.585630E-03
# Covariance matrix:
  2.7261E-13 -3.6247E-13  1.6234E-14 -4.7703E-14 -1.6802E-13 -3.8871E-12
 -3.6247E-13  8.0969E-13 -4.6556E-14  1.3690E-13  4.2776E-13  1.1159E-11
  1.6234E-14 -4.6556E-14  1.8341E-13 -1.1711E-13 -2.6943E-14 -7.1750E-13
 -4.7703E-14  1.3690E-13 -1.1711E-13  1.1075E-13  7.9039E-14  2.1101E-12
 -1.6802E-13  4.2776E-13 -2.6943E-14  7.9039E-14  3.5809E-13  6.4347E-12
 -3.8871E-12  1.1159E-11 -7.1750E-13  2.1101E-12  6.4347E-12  1.7201E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.424936   48.854754   -0.096737   -0.007157   -0.984709  2456978.782278
# Heliocentric elements and errors
Epoch:              2456970.5000  =  2014/11/09
Mean Anomaly:          327.90165 +/-     0.100
Argument of Peri:       40.09957 +/-     0.147
Long of Asc Node:       51.22239 +/-     0.000
Inclination:            10.57925 +/-     0.001
Eccentricity:         0.14419559 +/-    0.0003
Semi-Major Axis:     42.60888621 +/-    0.0055
Time of Perihelion: 2466028.4296 +/-      28.3
Perihelion:          36.46487260 +/-    0.0150
Aphelion:            48.75289983 +/-    0.0156
Period (y)              278.1368 +/-      0.05
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           24.73270570 +/-    0.0005
Ecliptic Y           28.45857369 +/-    0.0006
Ecliptic Z           -0.27223738 +/-    0.0000
Ecliptic XDOT        -0.00235369 +/-    0.0000
Ecliptic YDOT         0.00170796 +/-    0.0000
Ecliptic ZDOT         0.00054249 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   37.70505618 +/-    0.0006
Geocenter to KBO     36.72114649 +/-    0.0008
# Hcoef:  8.67

The following table shows the complete astrometric record for 15VQ170. 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 (15VQ170) followed by the observatory code and reference code for the source of the astrometry.

2014 11  17.28150  03 06 04.937  +17 01 17.50  24.7r 15VQ170   568  C~2nw6      
2014 11  17.39021  03 06 04.338  +17 01 15.44  25.0r 15VQ170   568  C~2nw6      
2014 11  17.50402  03 06 03.701  +17 01 13.26  24.6r 15VQ170   568  C~2nw6      
2014 11  19.29385  03 05 53.928  +17 00 39.16  23.4r 15VQ170   568  C~2nw6      
2014 11  23.39737  03 05 31.715  +16 59 21.83  24.0r 15VQ170   568  C~2nw6      
2015 09  07.62902  03 17 22.822  +18 01 38.22  24.6w 15VQ170   568  C~2nw6      
2015 09  12.49264  03 17 14.227  +18 01 19.07  24.7w 15VQ170   568  C~2nw6      
2015 10  07.53854  03 15 55.155  +17 57 28.49  24.6w 15VQ170   568  C~2nw6      
2015 10  07.59790  03 15 54.894  +17 57 27.75  24.8w 15VQ170   568  C~2nw6      
2015 10  09.57780  03 15 46.478  +17 57 01.04  24.6w 15VQ170   568  C~2nw6      
2015 11  07.33264  03 13 21.166  +17 49 04.52  24.2r 15VQ170   568  C~2nw6      
2015 11  07.37479  03 13 20.934  +17 49 03.77  24.2r 15VQ170   568  C~2nw6      
2015 11  07.41697  03 13 20.689  +17 49 03.00  24.4r 15VQ170   568  C~2nw6      
2015 11  17.34635  03 12 25.540  +17 45 57.85  24.5w 15VQ170   568  C~2nw6      
2015 11  17.39294  03 12 25.270  +17 45 57.02  24.6w 15VQ170   568  C~2nw6      
2015 12  06.35508  03 10 44.121  +17 40 17.92  24.7w 15VQ170   568  C~2nw6      
2015 12  06.49265  03 10 43.428  +17 40 15.84  24.8w 15VQ170   568  C~2nw6      
2016 01  01.36607  03 08 55.702  +17 34 29.62  24.4w 15VQ170   568  C~2nw6      
2016 02  04.28927  03 08 07.326  +17 33 04.34  24.9w 15VQ170   568  C~2nw6      
2016 02  10.27908  03 08 11.828  +17 33 41.38  24.4w 15VQ170   568  C~2nw6      
2016 09  07.57363  03 23 42.142  +18 44 21.00        15VQ170   568  C~2nw6      
2016 09  27.51061  03 22 53.726  +18 42 28.85  24.7w 15VQ170   568  C~2nw6      
2016 09  29.48481  03 22 46.931  +18 42 10.35  24.9w 15VQ170   568  C~2nw6      
2016 10  05.48792  03 22 24.277  +18 41 06.50  24.7w 15VQ170   568  C~2nw6      
2016 10  07.49247  03 22 16.097  +18 40 42.73  24.8w 15VQ170   568  C~2nw6      
2016 10  07.58817  03 22 15.684  +18 40 41.52  24.6w 15VQ170   568  C~2nw6      
2016 10  09.49252  03 22 07.634  +18 40 17.96  24.9w 15VQ170   568  C~2nw6      
2016 10  09.56525  03 22 07.308  +18 40 17.07  24.7w 15VQ170   568  C~2nw6      
2016 11  04.40663  03 19 57.852  +18 33 37.97  24.5w 15VQ170   568  C~2nw6      
2016 12  24.30698  03 15 41.093  +18 19 53.28  24.5w 15VQ170   568  C~2nw6      
2016 12  24.32550  03 15 41.003  +18 19 52.89  24.3w 15VQ170   568  C~2nw6      
2017 01  02.40920  03 15 08.734  +18 18 14.35  24.8w 15VQ170   568  C~2nw6      
2017 01  02.42780  03 15 08.665  +18 18 14.16  24.6w 15VQ170   568  C~2nw6      
2017 01  26.29981  03 14 22.108  +18 16 19.64  24.6w 15VQ170   568  C~2nw6      
2017 01  27.27995  03 14 21.507  +18 16 19.88  24.8w 15VQ170   568  C~2nw6      

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    -0.06       0.00    -0.02
     2   0.0003     -8.83     0.03       0.37    -0.04
     3   0.0006    -18.21    -0.01       0.77    -0.02
     4   0.0055   -162.37    -0.11       6.36     0.03
     5   0.0167   -490.00     0.07      19.36    -0.05
     6   0.8059  10319.16    -0.04     904.98     0.03
     7   0.8192  10195.49    -0.10     918.31    -0.04
     8   0.8878   9043.77    -0.07     989.44     0.01
     9   0.8879   9039.97    -0.15     989.69     0.09
    10   0.8934   8916.84    -0.06     995.29    -0.07
    11   0.9721   6787.07     0.16    1081.01     0.05
    12   0.9722   6783.67     0.23    1081.17     0.05
    13   0.9723   6780.09     0.12    1081.35     0.08
    14   0.9995   5970.74     0.03    1111.64    -0.02
    15   0.9996   5966.79    -0.06    1111.86     0.04
    16   1.0515   4482.47     0.02    1170.60    -0.04
    17   1.0519   4472.37     0.18    1171.25     0.16
    18   1.1228   2895.42    -0.05    1252.06    -0.01
    19   1.2156   2206.23    -0.07    1357.19    -0.04
    20   1.2320   2278.25    -0.00    1375.40    -0.11
    21   1.8078  16218.89     0.00    2008.73     0.04
    22   1.8624  15520.87    -0.03    2073.07    -0.03
    23   1.8678  15422.22     0.01    2079.49     0.02
    24   1.8842  15092.85    -0.01    2098.88     0.04
    25   1.8897  14973.74     0.09    2105.23    -0.06
    26   1.8900  14967.73     0.01    2105.54    -0.09
    27   1.8952  14850.48     0.05    2111.65    -0.06
    28   1.8954  14845.75    -0.03    2111.96    -0.01
    29   1.9661  12955.90     0.03    2193.76     0.01
    30   2.1027   9202.34     0.10    2341.31     0.04
    31   2.1028   9200.99    -0.16    2341.27    -0.06
    32   2.1277   8730.80     0.00    2366.38    -0.00
    33   2.1277   8729.80    -0.12    2366.45     0.02
    34   2.1931   8058.78    -0.06    2430.02     0.05
    35   2.1958   8050.58     0.04    2432.50    -0.01

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.

15VQ170    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        42.918    42.930    42.907
ecceobj         0.146     0.147     0.146
incobj         10.550    10.550    10.550
qmin           35.682    35.510    35.952
qmax           49.743    49.970    49.513
amean          42.524    42.537    42.508
amin           42.125    42.138    42.125
amax           42.931    42.956    42.927
emean           0.123     0.126     0.114
emin            0.093     0.097     0.079
emax            0.159     0.164     0.154
imean           8.007     7.954     7.979
imin            6.116     6.354     5.724
imax            9.829     9.823     9.831
excite_mean     0.186     0.188     0.181
fracstop        1.000     1.000     1.000
cjmean          3.043     3.042     3.045

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       178.1     178.1     177.8
kozaiamp        179.9     180.0     180.0