Orbit Fit and Astrometric record for 05EP296

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: 05EP296   
# Created Thu Nov 21 02:08:46 2024
# Orbit generated from Bernstein formalism
# Fitting      5 observations of      5
# Arc:  91.75d
# First observation: 2005/03/09
#  Last observation: 2005/06/09
Preliminary a, adot, b, bdot, g, gdot:
   0.000001   0.026849   0.000004   0.001281   0.023646   0.000000
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# WARNING Fitting with energy constraint
# Chi-squared of fit:    35.63 DOF:      5 RMS:  0.47
# Min/Max residuals:    -0.79    1.11
# Exact a, adot, b, bdot, g, gdot:
  1.714052E-05  2.428546E-02  4.673326E-06  1.225382E-03  2.323308E-02  2.259993E-04
# Covariance matrix:
  1.4409E-12  6.2279E-10 -2.7710E-16  1.6709E-11  1.8633E-10 -4.8778E-09
  6.2279E-10  4.6611E-07 -4.1757E-13  1.1945E-08  1.2516E-07 -7.2262E-06
 -2.7710E-16 -4.1757E-13  4.9092E-13 -1.9730E-12 -6.5560E-14  1.8543E-11
  1.6709E-11  1.1945E-08 -1.9730E-12  3.3067E-10  3.3227E-09 -1.5543E-07
  1.8633E-10  1.2516E-07 -6.5560E-14  3.3227E-09  3.6670E-08 -1.1481E-06
 -4.8778E-09 -7.2262E-06  1.8543E-11 -1.5543E-07 -1.1481E-06  3.1736E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
    1.046647  156.419555   -0.209688    0.017744   -0.966154  2453438.775183
# Heliocentric elements and errors
Epoch:              2453430.5000  =  2005/03/01
Mean Anomaly:            2.45877 +/-   138.557
Argument of Peri:       15.54178 +/-   226.449
Long of Asc Node:      137.14006 +/-     0.389
Inclination:             3.05617 +/-     0.059
Eccentricity:         0.22728765 +/-    0.0360
Semi-Major Axis:     56.93241098 +/-    1.8580
Time of Perihelion: 2452358.8509 +/-   60389.7
Perihelion:          43.99237710 +/-    2.5037
Aphelion:            69.87244486 +/-    3.0671
Period (y)              429.5835 +/-     21.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -40.41557179 +/-    0.3251
Ecliptic Y           17.40904062 +/-    0.1419
Ecliptic Z            0.78644026 +/-    0.0065
Ecliptic XDOT        -0.00116676 +/-    0.0019
Ecliptic YDOT        -0.00262045 +/-    0.0009
Ecliptic ZDOT         0.00014493 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   44.01263031 +/-    0.3037
Geocenter to KBO     43.04207932 +/-    0.3548
# Hcoef:  7.51

The following table shows the complete astrometric record for 05EP296. 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 (05EP296) followed by the observatory code and reference code for the source of the astrometry.

2005 03  09.27444  10 34 16.37   +10 07 42.9   23.9R 05EP296   695  Cn0309      
2005 03  09.36686  10 34 16.00   +10 07 45.6         05EP296   695  Cn0309      
2005 03  10.27160  10 34 12.20   +10 08 09.9         05EP296   695  Cn0309      
2005 06  08.97715  10 31 42.96   +10 22 02.4   23.4R 05EP296   304  Cn7066      
2005 06  09.02829  10 31 43.03   +10 22 02.4         05EP296   304  Cn7066      

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    -0.13       0.00    -0.79
     2   0.0003     -6.07     0.14       0.48    -0.30
     3   0.0027    -67.20    -0.01       2.28     1.11
     4   0.2511  -2421.89     0.26     -37.82    -0.23
     5   0.2512  -2420.92    -0.26     -37.44     0.21

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.

05EP296    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