Orbit Fit and Astrometric record for 05JA186

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: 05JA186   
# Created Sat Apr 20 01:12:26 2024
# Orbit generated from Bernstein formalism
# Fitting      7 observations of      7
# Arc:  17.99d
# First observation: 2005/05/14
#  Last observation: 2005/06/01
Preliminary a, adot, b, bdot, g, gdot:
   0.000001   0.018783  -0.000000  -0.001549   0.022641   0.000000
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# WARNING Fitting with energy constraint
# Chi-squared of fit:    14.31 DOF:      9 RMS:  0.25
# Min/Max residuals:    -0.53    0.53
# Exact a, adot, b, bdot, g, gdot:
  1.174584E-05  1.509436E-02 -1.284772E-06 -1.523749E-03  2.204465E-02 -1.380374E-02
# Covariance matrix:
  1.4657E-11  1.7846E-08  1.0026E-13 -1.3012E-10  2.9886E-09  5.4810E-09
  1.7846E-08  2.2168E-05  1.2441E-10 -1.6150E-07  3.7100E-06  5.8587E-06
  1.0026E-13  1.2441E-10  2.6923E-13 -7.6325E-12  2.0826E-11  3.7545E-11
 -1.3012E-10 -1.6150E-07 -7.6325E-12  1.9487E-09 -2.7033E-08 -4.6702E-08
  2.9886E-09  3.7100E-06  2.0826E-11 -2.7033E-08  6.2098E-07  1.0342E-06
  5.4810E-09  5.8587E-06  3.7545E-11 -4.6702E-08  1.0342E-06  5.6744E-05
#      lat0       lon0       xBary       yBary       zBary        JD0
   -1.657760 -132.236278   -0.105465   -0.028910   -1.001763  2453504.874123
# Heliocentric elements and errors
Epoch:              2453500.5000  =  2005/05/10
Mean Anomaly:          309.81699 +/-    42.078
Argument of Peri:      326.83785 +/-    23.182
Long of Asc Node:       32.04761 +/-     4.322
Inclination:             5.92092 +/-     1.569
Eccentricity:         0.66947256 +/-    0.2524
Semi-Major Axis:     47.18651015 +/-   24.4812
Time of Perihelion: 2470004.1265 +/-    5151.7
Perihelion:          15.59643649 +/-   14.3995
Aphelion:            78.77658381 +/-   42.5709
Period (y)              324.1418 +/-    252.26
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -31.07887832 +/-    1.0897
Ecliptic Y          -34.38526597 +/-    1.2000
Ecliptic Z           -1.31233527 +/-    0.0469
Ecliptic XDOT         0.00254423 +/-    0.0007
Ecliptic YDOT         0.00000562 +/-    0.0009
Ecliptic ZDOT        -0.00013952 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   46.36771956 +/-    1.1512
Geocenter to KBO     45.36247059 +/-    1.6216
# Hcoef:  6.90

The following table shows the complete astrometric record for 05JA186. 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 (05JA186) followed by the observatory code and reference code for the source of the astrometry.

2005 05  14.37338  14 59 14.67   -18 43 07.9   23.5r 05JA186   568  C~0D3W      
2005 05  14.40709  14 59 14.51   -18 43 07.4   23.5r 05JA186   568  C~0D3W      
2005 05  14.44596  14 59 14.33   -18 43 06.8   23.5r 05JA186   568  C~0D3W      
2005 05  15.463184 14 59 09.66   -18 42 47.7         05JA186   T14  C~63QJ      
2005 05  16.359309 14 59 05.52   -18 42 30.8         05JA186   T14  C~63QJ      
2005 05  17.34300  14 59 00.92   -18 42 12.2   23.2r 05JA186   568  C~0D3W      
2005 06  01.362884 14 57 54.33   -18 37 37.0         05JA186   T14  C~63QJ      

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    -0.19       0.00     0.04
     2   0.0001     -2.32    -0.16      -0.16    -0.09
     3   0.0002     -4.94    -0.08      -0.31    -0.20
     4   0.0030    -73.98     0.53      -0.72     0.05
     5   0.0054   -135.18     0.42      -1.12     0.15
     6   0.0081   -203.13    -0.53      -1.75     0.08
     7   0.0493  -1188.65     0.01      -5.98    -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.

05JA186    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