Orbit Fit and Astrometric record for 15VL170

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: 15VL170   
# Created Tue Apr 23 01:17:40 2024
# Orbit generated from Bernstein formalism
# Fitting     34 observations of     34
# Arc:   2.32y
# First observation: 2015/08/20
#  Last observation: 2017/12/13
Preliminary a, adot, b, bdot, g, gdot:
  -0.000132   0.025456  -0.000007   0.012859   0.026884   0.000000
# Chi-squared of fit:     6.46 DOF:     62 RMS:  0.08
# Min/Max residuals:    -0.18    0.19
# Exact a, adot, b, bdot, g, gdot:
  1.500996E-05  2.501564E-02  8.043210E-06  1.263932E-02  2.659144E-02  6.253078E-04
# Covariance matrix:
  1.7506E-13 -4.0946E-14 -4.8371E-15  2.3514E-14  1.0753E-13  9.0641E-13
 -4.0946E-14  2.8919E-13 -4.6083E-14  1.7442E-13  1.4411E-13  6.5264E-12
 -4.8371E-15 -4.6083E-14  1.0577E-13 -1.0904E-13 -3.1329E-14 -1.5018E-12
  2.3514E-14  1.7442E-13 -1.0904E-13  2.4083E-13  1.2456E-13  5.6839E-12
  1.0753E-13  1.4411E-13 -3.1329E-14  1.2456E-13  2.0422E-13  4.6914E-12
  9.0641E-13  6.5264E-12 -1.5018E-12  5.6839E-12  4.6914E-12  2.1268E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
   -1.589851   53.457974    1.012502   -0.001677   -0.065167  2457255.056669
# Heliocentric elements and errors
Epoch:              2457250.5000  =  2015/08/16
Mean Anomaly:          356.59190 +/-     0.471
Argument of Peri:        0.30825 +/-     0.531
Long of Asc Node:       55.06233 +/-     0.000
Inclination:            26.81823 +/-     0.001
Eccentricity:         0.05948309 +/-    0.0000
Semi-Major Axis:     40.06045226 +/-    0.0024
Time of Perihelion: 2458127.2618 +/-     121.1
Perihelion:          37.67753276 +/-    0.0029
Aphelion:            42.44337176 +/-    0.0031
Period (y)              253.5607 +/-      0.02
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           23.23079497 +/-    0.0004
Ecliptic Y           29.65120537 +/-    0.0005
Ecliptic Z           -1.04303901 +/-    0.0000
Ecliptic XDOT        -0.00201147 +/-    0.0000
Ecliptic YDOT         0.00160789 +/-    0.0000
Ecliptic ZDOT         0.00129911 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   37.68224708 +/-    0.0005
Geocenter to KBO     37.60608457 +/-    0.0006
# Hcoef:  8.47

The following table shows the complete astrometric record for 15VL170. 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 (15VL170) followed by the observatory code and reference code for the source of the astrometry.

2015 08  20.55588  03 25 56.673  +17 05 52.18  24.5w 15VL170   568  C~2nw5      
2015 09  07.60452  03 25 46.771  +17 06 42.85  24.6w 15VL170   568  C~2nw5      
2015 09  12.45550  03 25 38.321  +17 06 36.20  24.7w 15VL170   568  C~2nw5      
2015 10  07.50351  03 24 19.186  +17 04 00.53  24.4w 15VL170   568  C~2nw5      
2015 10  07.56195  03 24 18.932  +17 03 59.91  24.5w 15VL170   568  C~2nw5      
2015 10  09.54258  03 24 10.437  +17 03 40.15  24.5w 15VL170   568  C~2nw5      
2015 11  06.33883  03 21 47.889  +16 57 50.27  24.1r 15VL170   568  C~2nw5      
2015 11  06.40946  03 21 47.493  +16 57 49.51  24.4r 15VL170   568  C~2nw5      
2015 11  06.47899  03 21 47.085  +16 57 48.54  24.0r 15VL170   568  C~2nw5      
2015 11  07.49597  03 21 41.316  +16 57 33.92  24.4w 15VL170   568  C~2nw5      
2015 11  17.47779  03 20 44.157  +16 55 12.97  24.3w 15VL170   568  C~2nw5      
2015 11  17.56554  03 20 43.640  +16 55 11.78  24.2w 15VL170   568  C~2nw5      
2015 12  06.34344  03 18 59.154  +16 51 06.72  24.4w 15VL170   568  C~2nw5      
2015 12  06.48092  03 18 58.428  +16 51 05.14  24.3w 15VL170   568  C~2nw5      
2015 12  31.35875  03 17 05.975  +16 47 34.94  24.3w 15VL170   568  C~2nw5      
2016 01  07.39390  03 16 42.884  +16 47 11.34  24.3w 15VL170   568  C~2nw5      
2016 01  08.24465  03 16 40.414  +16 47 09.69  24.5w 15VL170   568  C~2nw5      
2016 02  04.37827  03 16 00.728  +16 48 54.24  24.4w 15VL170   568  C~2nw5      
2016 02  11.24103  03 16 03.465  +16 50 10.36  24.6w 15VL170   568  C~2nw5      
2016 09  07.59099  03 30 52.990  +18 10 20.77  24.5w 15VL170   568  C~2nw5      
2016 09  27.52301  03 30 04.212  +18 09 32.39  24.5w 15VL170   568  C~2nw5      
2016 10  05.50531  03 29 34.409  +18 08 38.48  24.8w 15VL170   568  C~2nw5      
2016 10  07.50982  03 29 26.135  +18 08 22.05  24.3w 15VL170   568  C~2nw5      
2016 10  07.60551  03 29 25.713  +18 08 21.06  24.5w 15VL170   568  C~2nw5      
2016 10  09.51019  03 29 17.546  +18 08 04.74  24.4w 15VL170   568  C~2nw5      
2016 10  09.58259  03 29 17.227  +18 08 04.09  24.4w 15VL170   568  C~2nw5      
2016 11  02.47946  03 27 16.192  +18 03 35.47  24.6w 15VL170   568  C~2nw5      
2016 11  04.45547  03 27 05.093  +18 03 09.61  24.6w 15VL170   568  C~2nw5      
2016 12  28.44773  03 22 20.380  +17 52 47.27  24.4w 15VL170   568  C~2nw5      
2017 01  27.29772  03 21 05.863  +17 52 17.03  24.5w 15VL170   568  C~2nw5      
2017 09  15.55809  03 35 50.266  +19 13 33.84        15VL170   568  C~2nw5      
2017 09  20.60688  03 35 38.251  +19 13 29.76  24.4w 15VL170   568  C~2nw5      
2017 12  13.36234  03 28 41.066  +18 59 39.99  24.7w 15VL170   568  C~2nw5      
2017 12  13.40466  03 28 40.842  +18 59 39.46  24.4w 15VL170   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    -0.03       0.00    -0.11
     2   0.0494   -124.97    -0.13      84.28    -0.01
     3   0.0627   -243.97    -0.08     107.89     0.12
     4   0.1313  -1381.64    -0.01     239.64     0.03
     5   0.1314  -1385.32    -0.05     239.95    -0.01
     6   0.1369  -1508.22     0.04     251.26    -0.02
     7   0.2130  -3575.48    -0.02     426.80    -0.02
     8   0.2132  -3581.18     0.17     427.50     0.15
     9   0.2133  -3587.09     0.06     428.05     0.19
    10   0.2161  -3670.89    -0.06     434.84    -0.08
    11   0.2435  -4500.33    -0.10     506.57    -0.04
    12   0.2437  -4507.81    -0.18     507.31     0.05
    13   0.2951  -6021.40     0.00     653.36    -0.06
    14   0.2955  -6031.89     0.17     654.50    -0.06
    15   0.3636  -7647.98    -0.00     867.43    -0.03
    16   0.3829  -7974.86     0.07     930.56    -0.02
    17   0.3852  -8009.60     0.01     938.17    -0.07
    18   0.4595  -8533.67     0.03    1187.34    -0.10
    19   0.4783  -8475.84    -0.03    1250.68     0.01
    20   1.0514   5054.86     0.12    2715.37    -0.01
    21   1.1060   4368.21     0.03    2836.60    -0.00
    22   1.1279   3942.83    -0.04    2887.42     0.19
    23   1.1333   3824.38     0.18    2900.16     0.01
    24   1.1336   3818.30     0.01    2900.66    -0.13
    25   1.1388   3701.37    -0.01    2913.16     0.04
    26   1.1390   3696.80     0.04    2913.64     0.03
    27   1.2044   1957.33    -0.05    3075.54     0.04
    28   1.2099   1797.52     0.06    3089.44    -0.02
    29   1.3577  -2292.45     0.03    3499.93    -0.03
    30   1.4394  -3329.63    -0.12    3740.20    -0.04
    31   2.0726  10069.26    -0.01    5398.33    -0.00
    32   2.0864   9902.47    -0.03    5434.29    -0.01
    33   2.3157   3953.87     0.00    6043.59     0.03
    34   2.3158   3950.65    -0.07    6043.85    -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.

15VL170    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        40.409    40.419    40.399
ecceobj         0.067     0.067     0.066
incobj         26.731    26.731    26.732
qmin           36.901    36.991    36.945
qmax           43.432    43.489    43.487
amean          40.123    40.115    40.111
amin           39.813    39.802    39.785
amax           40.446    40.447    40.442
emean           0.062     0.063     0.063
emin            0.050     0.051     0.050
emax            0.075     0.076     0.076
imean          25.508    25.502    25.503
imin           25.061    25.058    25.057
imax           26.010    25.997    25.999
excite_mean     0.435     0.435     0.435
fracstop        1.000     1.000     1.000
cjmean          2.831     2.831     2.831

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       169.3     169.3     169.4
kozaiamp        180.0     179.9     180.0