Orbit Fit and Astrometric record for VNH0015

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: VNH0015   
# Created Wed Jun  4 01:12:16 2025
# Orbit generated from Bernstein formalism
# Fitting      6 observations of      6
# Arc:   5.10d
# First observation: 2011/04/28
#  Last observation: 2011/05/03
# WARNING Fitting with energy constraint
# WARNING and with gdot fixed = 0
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# Chi-squared of fit:     0.51 DOF:      8 RMS:  0.05
# Min/Max residuals:    -0.12    0.06
# Exact a, adot, b, bdot, g, gdot:
  1.653223E-05  3.069912E-02  5.808005E-06  1.041716E-02  2.981042E-02  0.000000E+00
# Covariance matrix:
  3.4267E-10  6.5935E-07 -2.3265E-11 -4.3939E-08  2.0274E-07  0.0000E+00
  6.5935E-07  1.2706E-03 -4.4830E-08 -8.4666E-05  3.9066E-04  0.0000E+00
 -2.3265E-11 -4.4830E-08  2.0513E-12  2.9529E-09 -1.3784E-08  0.0000E+00
 -4.3939E-08 -8.4666E-05  2.9529E-09  5.6470E-06 -2.6032E-05  0.0000E+00
  2.0274E-07  3.9066E-04 -1.3784E-08 -2.6032E-05  1.2011E-04  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  3.4860E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
    2.320498  -82.280641    0.878083    0.020177   -0.498486  2455679.747046
# Heliocentric elements and errors
Epoch:              2455670.5000  =  2011/04/19
Mean Anomaly:          307.90183 +/-   316.652
Argument of Peri:       62.16356 +/-    17.185
Long of Asc Node:      269.57326 +/-     9.651
Inclination:            18.95421 +/-    24.037
Eccentricity:         0.03297645 +/-    0.7403
Semi-Major Axis:     34.73570841 +/-   21.3197
Time of Perihelion: 2466491.8788 +/-  289929.3
Perihelion:          33.59024817 +/-   32.9602
Aphelion:            35.88116866 +/-   33.8575
Period (y)              204.7257 +/-    188.48
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X            3.70359785 +/-    1.6548
Ecliptic Y          -33.82630017 +/-   12.2110
Ecliptic Z            1.35842911 +/-    0.4995
Ecliptic XDOT         0.00278682 +/-    0.0022
Ecliptic YDOT         0.00042304 +/-    0.0017
Ecliptic ZDOT         0.00095598 +/-    0.0006
# Distances at JD0 (AU)
Heliocenter to KBO   34.05555094 +/-   12.1301
Geocenter to KBO     33.54531391 +/-   12.3327
# Hcoef: 10.43

The following table shows the complete astrometric record for VNH0015. 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 (VNH0015) followed by the observatory code and reference code for the source of the astrometry.

2011 04  28.24628  18 33 02.341  -20 53 51.84        VNH0015   304              
2011 04  28.34249  18 33 02.104  -20 53 51.04        VNH0015   304              
2011 04  28.41932  18 33 01.910  -20 53 50.43        VNH0015   304              
2011 05  03.28524  18 32 48.746  -20 53 14.57        VNH0015   304              
2011 05  03.30874  18 32 48.661  -20 53 14.39        VNH0015   304              
2011 05  03.34419  18 32 48.565  -20 53 14.13  25.5R VNH0015   304              

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    -0.06
     2   0.0003     -3.27     0.02       0.99     0.02
     3   0.0005     -5.95     0.03       1.75     0.04
     4   0.0138   -188.08     0.06      48.07    -0.02
     5   0.0139   -189.26    -0.12      48.32     0.01
     6   0.0140   -190.59     0.06      48.66     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.

VNH0015    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