Orbit Fit and Astrometric record for 01OL108

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: 01OL108   
# Created Fri Nov  1 01:08:07 2024
# Orbit generated from Bernstein formalism
# Fitting      6 observations of      6
# Arc: 113.69d
# First observation: 2001/07/24
#  Last observation: 2001/11/15
Preliminary a, adot, b, bdot, g, gdot:
   0.000000   0.028904   0.000001  -0.001209   0.025506   0.000000
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# WARNING Fitting with energy constraint
# Chi-squared of fit:     1.99 DOF:      7 RMS:  0.10
# Min/Max residuals:    -0.13    0.24
# Exact a, adot, b, bdot, g, gdot:
  1.628172E-05  2.524164E-02 -1.484491E-07 -1.197566E-03  2.491482E-02 -1.949495E-03
# Covariance matrix:
  1.3727E-12  1.1280E-09  1.3268E-15 -6.6221E-12  2.3851E-10 -2.1836E-08
  1.1280E-09  1.4653E-06  1.3825E-12 -6.7204E-09  2.7454E-07 -3.4918E-05
  1.3268E-15  1.3825E-12  3.6769E-13 -1.1946E-12  3.1125E-13 -2.3114E-11
 -6.6221E-12 -6.7204E-09 -1.1946E-12  5.8198E-11 -1.5475E-09  1.0588E-07
  2.3851E-10  2.7454E-07  3.1125E-13 -1.5475E-09  5.6822E-08 -5.5291E-06
 -2.1836E-08 -3.4918E-05 -2.3114E-11  1.0588E-07 -5.5291E-06  1.0229E-03
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.484455  -54.526128    0.075678   -0.008739   -1.016134  2452114.868983
# Heliocentric elements and errors
Epoch:              2452110.5000  =  2001/07/20
Mean Anomaly:          317.26657 +/-   279.877
Argument of Peri:      242.03164 +/-    47.131
Long of Asc Node:      115.52740 +/-     0.451
Inclination:             2.75996 +/-     0.125
Eccentricity:         0.10987496 +/-    1.1114
Semi-Major Axis:     44.45992626 +/-   13.4506
Time of Perihelion: 2464963.8646 +/-   83979.2
Perihelion:          39.57489357 +/-   50.8409
Aphelion:            49.34495894 +/-   51.6169
Period (y)              296.4567 +/-    134.53
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           23.82333558 +/-    0.2228
Ecliptic Y          -33.55101070 +/-    0.3127
Ecliptic Z           -0.33934019 +/-    0.0032
Ecliptic XDOT         0.00212536 +/-    0.0020
Ecliptic YDOT         0.00178673 +/-    0.0029
Ecliptic ZDOT        -0.00012958 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   41.15017362 +/-    0.2858
Geocenter to KBO     40.13674622 +/-    0.3840
# Hcoef:  8.40

The following table shows the complete astrometric record for 01OL108. 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 (01OL108) followed by the observatory code and reference code for the source of the astrometry.

2001 07  24.36824  20 31 50.80   -19 22 16.5   24.3R 01OL108   568  Cd3420      
2001 07  24.40897  20 31 50.60   -19 22 17.1   24.0R 01OL108   568  Cd3420      
2001 07  24.44993  20 31 50.39   -19 22 18.0   24.0R 01OL108   568  Cd3420      
2001 07  25.44308  20 31 45.45   -19 22 36.0         01OL108   568  Cd3420      
2001 11  15.01195  20 27 51.72   -19 36 38.8   24.4R 01OL108   309  Ce3591      
2001 11  15.05952  20 27 51.87   -19 36 38.4         01OL108   309  Ce3591      

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    -0.13
     2   0.0001     -2.89     0.06       0.11     0.01
     3   0.0002     -5.99    -0.01      -0.03    -0.12
     4   0.0029    -78.18     0.00      -0.39     0.24
     5   0.3111  -3489.20    -0.10     -18.95     0.07
     6   0.3113  -3487.05     0.10     -19.07    -0.07

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.

01OL108    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