Orbit Fit and Astrometric record for 05EJ300

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: 05EJ300   
# Created Wed Dec  4 02:08:43 2024
# Orbit generated from Bernstein formalism
# Fitting      5 observations of      5
# Arc:  31.97d
# First observation: 2005/03/11
#  Last observation: 2005/04/12
Preliminary a, adot, b, bdot, g, gdot:
   0.000000   0.022210   0.000000   0.008311   0.023832   0.000000
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# WARNING Fitting with energy constraint
# Chi-squared of fit:     1.11 DOF:      5 RMS:  0.08
# Min/Max residuals:    -0.16    0.17
# Exact a, adot, b, bdot, g, gdot:
  1.183614E-05  1.714034E-02  5.698233E-06  8.403510E-03  2.302351E-02 -1.085577E-02
# Covariance matrix:
  1.9286E-11  2.1260E-08  9.8023E-14 -2.2449E-10  3.7650E-09  1.1664E-08
  2.1260E-08  2.4133E-05  1.1361E-10 -2.5671E-07  4.2682E-06  1.0671E-05
  9.8023E-14  1.1361E-10  5.0343E-13 -7.1954E-12  1.9904E-11 -5.6831E-11
 -2.2449E-10 -2.5671E-07 -7.1954E-12  2.9654E-09 -4.5246E-08 -2.5503E-08
  3.7650E-09  4.2682E-06  1.9904E-11 -4.5246E-08  7.5523E-07  2.0930E-06
  1.1664E-08  1.0671E-05 -5.6831E-11 -2.5503E-08  2.0930E-06  1.2045E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
   -1.494705  162.514936   -0.140680   -0.025452   -0.978926  2453440.795683
# Heliocentric elements and errors
Epoch:              2453440.5000  =  2005/03/11
Mean Anomaly:          301.47372 +/-    55.717
Argument of Peri:      113.18538 +/-    35.605
Long of Asc Node:      165.68959 +/-     0.874
Inclination:            26.05673 +/-     6.566
Eccentricity:         0.49187778 +/-    0.4207
Semi-Major Axis:     45.72750187 +/-   24.0391
Time of Perihelion: 2471802.2063 +/-    9793.6
Perihelion:          23.23515991 +/-   22.7882
Aphelion:            68.21984383 +/-   40.6975
Period (y)              309.2249 +/-    243.84
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -42.39366536 +/-    1.5631
Ecliptic Y           13.20493048 +/-    0.4926
Ecliptic Z           -1.13268997 +/-    0.0428
Ecliptic XDOT         0.00059368 +/-    0.0013
Ecliptic YDOT        -0.00233112 +/-    0.0006
Ecliptic ZDOT         0.00103270 +/-    0.0001
# Distances at JD0 (AU)
Heliocenter to KBO   44.41706922 +/-    1.4991
Geocenter to KBO     43.43385599 +/-    1.6394
# Hcoef:  7.92

The following table shows the complete astrometric record for 05EJ300. 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 (05EJ300) followed by the observatory code and reference code for the source of the astrometry.

2005 03  11.29494  10 53 13.44   +05 28 57.1   23.8R 05EJ300   695  Cn0311      
2005 03  12.25253  10 53 09.32   +05 29 27.6         05EJ300   695  Cn0311      
2005 03  12.33534  10 53 08.94   +05 29 30.5         05EJ300   695  Cn0311      
2005 04  12.21587  10 51 10.66   +05 44 43.4   24.3R 05EJ300   695  Cn3133      
2005 04  12.26719  10 51 10.49   +05 44 44.7         05EJ300   695  Cn3133      

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     0.02
     2   0.0026    -68.50     0.17       4.75    -0.07
     3   0.0028    -74.85    -0.16       5.27     0.06
     4   0.0874  -2055.18     0.03     177.19     0.03
     5   0.0875  -2058.02    -0.03     177.42    -0.02

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.

05EJ300    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