Orbit Fit and Astrometric record for 15VY184

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: 15VY184   
# Created Fri Nov  1 01:10:19 2024
# Orbit generated from Bernstein formalism
# Fitting      5 observations of      5
# Arc:  31.95d
# First observation: 2015/11/07
#  Last observation: 2015/12/09
Preliminary a, adot, b, bdot, g, gdot:
   0.000000   0.051605  -0.000000   0.019349   0.037155   0.000000
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# WARNING Fitting with energy constraint
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# Chi-squared of fit:     2.87 DOF:      5 RMS:  0.13
# Min/Max residuals:    -0.30    0.29
# Exact a, adot, b, bdot, g, gdot:
  1.727539E-05  3.830171E-02  8.154890E-06  1.804614E-02  3.495674E-02  2.021120E-03
# Covariance matrix:
  4.3401E-11  8.7278E-08  2.7777E-12  9.3691E-09  1.6061E-08 -1.1410E-07
  8.7278E-08  1.7774E-04  5.6470E-09  1.9049E-05  3.2648E-05 -2.5645E-04
  2.7777E-12  5.6470E-09  6.6759E-13  6.0095E-10  1.0399E-09 -7.0625E-09
  9.3691E-09  1.9049E-05  6.0095E-10  2.0459E-06  3.5073E-06 -2.4070E-05
  1.6061E-08  3.2648E-05  1.0399E-09  3.5073E-06  6.0134E-06 -4.0285E-05
 -1.1410E-07 -2.5645E-04 -7.0625E-09 -2.4070E-05 -4.0285E-05  3.1815E-03
#      lat0       lon0       xBary       yBary       zBary        JD0
   10.383907   30.039379   -0.242672    0.174000   -0.948622  2457333.736799
# Heliocentric elements and errors
Epoch:              2457330.5000  =  2015/11/04
Mean Anomaly:           24.63903 +/-   186.575
Argument of Peri:      351.90933 +/-   345.878
Long of Asc Node:       10.19152 +/-     5.202
Inclination:            27.02425 +/-     5.772
Eccentricity:         0.11037234 +/-    0.6902
Semi-Major Axis:     32.75790368 +/-   12.3423
Time of Perihelion: 2452643.5143 +/-  103939.1
Perihelion:          29.14233727 +/-   25.1345
Aphelion:            36.37347009 +/-   26.4386
Period (y)              187.4918 +/-    105.96
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           25.06824780 +/-    1.7088
Ecliptic Y           14.77813191 +/-    0.9880
Ecliptic Z            5.15639096 +/-    0.3617
Ecliptic XDOT        -0.00158886 +/-    0.0039
Ecliptic YDOT         0.00254063 +/-    0.0020
Ecliptic ZDOT         0.00141882 +/-    0.0008
# Distances at JD0 (AU)
Heliocenter to KBO   29.55331789 +/-    1.5327
Geocenter to KBO     28.60678875 +/-    2.0068
# Hcoef:  9.76

The following table shows the complete astrometric record for 15VY184. 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 (15VY184) followed by the observatory code and reference code for the source of the astrometry.

2015 11  07.23601  01 36 12.860  +21 10 33.52  24.3r 15VY184   568  C~3wqO      
2015 11  07.33054  01 36 12.213  +21 10 30.42  24.4r 15VY184   568  C~3wqO      
2015 11  07.44914  01 36 11.405  +21 10 26.61  24.4r 15VY184   568  C~3wqO      
2015 12  09.16465  01 33 16.333  +20 53 21.02        15VY184   304  C~3wqO      
2015 12  09.18769  01 33 16.280  +20 53 20.50        15VY184   304  C~3wqO      

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     0.01       0.00     0.00
     2   0.0003     -9.55    -0.04       0.46    -0.03
     3   0.0006    -21.46     0.02       1.09     0.02
     4   0.0874  -2678.33    -0.30     -40.65     0.03
     5   0.0875  -2679.21     0.29     -40.86    -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.

15VY184    quality flag:0

Type:      ERR2LARGE ERR2LARGE ERR2LARGE

axisobj         0.000     0.000     0.000
ecceobj        -1.000    -1.000    -1.000
incobj         -1.000    -1.000    -1.000
qmin            0.000     0.000     0.000
qmax            0.000     0.000     0.000
amean           0.000     0.000     0.000
amin            0.000     0.000     0.000
amax            0.000     0.000     0.000
emean           0.000     0.000     0.000
emin            0.000     0.000     0.000
emax            0.000     0.000     0.000
imean           0.000     0.000     0.000
imin            0.000     0.000     0.000
imax            0.000     0.000     0.000
excite_mean     0.000     0.000     0.000
fracstop        0.000     0.000     0.000
cjmean          0.000     0.000     0.000

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         0.0       0.0       0.0
kozaiamp          0.0       0.0       0.0