Orbit Fit and Astrometric record for VNH0054

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: VNH0054   
# Created Wed Jun  4 01:12:17 2025
# Orbit generated from Bernstein formalism
# Fitting      6 observations of      6
# Arc:   1.07d
# First observation: 2012/04/17
#  Last observation: 2012/04/18
# WARNING Fitting with energy constraint
# WARNING and with gdot fixed = 0
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# Chi-squared of fit:     0.83 DOF:      8 RMS:  0.07
# Min/Max residuals:    -0.12    0.08
# Exact a, adot, b, bdot, g, gdot:
  1.464279E-05  2.045163E-02 -7.266122E-07 -7.113888E-04  2.191155E-02  0.000000E+00
# Covariance matrix:
 -1.4996E-10 -2.0816E-07  1.4171E-11  1.9620E-08 -1.0519E-07  0.0000E+00
 -2.0816E-07 -2.8748E-04  1.9598E-08  2.7134E-05 -1.4548E-04  0.0000E+00
  1.4171E-11  1.9598E-08 -8.9785E-13 -2.0207E-09  9.9120E-09  0.0000E+00
  1.9620E-08  2.7134E-05 -2.0207E-09 -2.4063E-06  1.3724E-05  0.0000E+00
 -1.0519E-07 -1.4548E-04  9.9120E-09  1.3724E-05 -7.3578E-05  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  1.3843E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
    1.798676  -81.309872    0.953063    0.010231   -0.325716  2456034.841006
# Heliocentric elements and errors
Epoch:              2456030.5000  =  2012/04/13
Mean Anomaly:          300.09297 +/-   315.020
Argument of Peri:      200.02369 +/-   200.024
Long of Asc Node:      139.91439 +/-   139.914
Inclination:             2.64658 +/-     2.647
Eccentricity:         0.02550693 +/-    0.4417
Semi-Major Axis:     46.54461905 +/-   46.5446
Time of Perihelion: 2475331.4155 +/- 9999999.9
Perihelion:          45.35740854 +/-   49.7986
Aphelion:            47.73182957 +/-   51.9705
Period (y)              317.5502 +/-    476.33
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X            6.00259243 +/-    6.0026
Ecliptic Y          -45.55612316 +/-  -45.5561
Ecliptic Z            1.43244585 +/-    1.4324
Ecliptic XDOT         0.00252156 +/-    0.0025
Ecliptic YDOT         0.00038702 +/-    0.0014
Ecliptic ZDOT        -0.00008874 +/-   -0.0001
# Distances at JD0 (AU)
Heliocenter to KBO   45.97220219 +/-   45.1506
Geocenter to KBO     45.63802334 +/-   45.6380
# Hcoef: 12.98

The following table shows the complete astrometric record for VNH0054. 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 (VNH0054) followed by the observatory code and reference code for the source of the astrometry.

2012 04  17.34024  18 37 19.665  -21 21 34.36  29.8R VNH0054   304              
2012 04  17.38698  18 37 19.616  -21 21 34.41  28.7R VNH0054   304              
2012 04  18.26735  18 37 18.811  -21 21 33.31        VNH0054   304              
2012 04  18.31518  18 37 18.762  -21 21 33.39  29.4R VNH0054   304              
2012 04  18.36209  18 37 18.700  -21 21 33.43  29.5R VNH0054   304              
2012 04  18.40587  18 37 18.661  -21 21 33.22  29.4R VNH0054   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     0.02       0.00     0.04
     2   0.0001     -0.69    -0.04      -0.01    -0.05
     3   0.0025    -11.84     0.07       1.82     0.08
     4   0.0027    -12.53     0.07       1.78    -0.03
     5   0.0028    -13.39    -0.12       1.80    -0.10
     6   0.0029    -13.92    -0.01       2.04     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.

VNH0054    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