Orbit Fit and Astrometric record for 119068

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: 119068    
# Created Thu Apr 18 01:07:21 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     21 observations of     21
# Arc:   3.97y
# First observation: 2001/05/23
#  Last observation: 2005/05/11
# Chi-squared of fit:    48.32 DOF:     36 RMS:  0.27
# Min/Max residuals:    -0.72    0.74
# Exact a, adot, b, bdot, g, gdot:
  1.988559E-05  3.487670E-02 -4.297834E-06 -7.989925E-03  2.907128E-02  1.249262E-04
# Covariance matrix:
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.260691 -121.154139   -0.057207   -0.004756   -1.017306  2452052.676443
# Heliocentric elements and errors
Epoch:              2452052.5000  =  2001/05/23
Mean Anomaly:            0.56999 +/-     0.000
Argument of Peri:      179.86055 +/-     0.000
Long of Asc Node:       57.83596 +/-     0.000
Inclination:            12.93388 +/-     0.000
Eccentricity:         0.35217332 +/-    0.0000
Semi-Major Axis:     54.65492399 +/-    0.0000
Time of Perihelion: 2451818.8284 +/-       0.0
Perihelion:          35.40691788 +/-    0.0000
Aphelion:            73.90293010 +/-    0.0000
Period (y)              404.0658 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -18.26876603 +/-    0.0000
Ecliptic Y          -30.33213523 +/-    0.0000
Ecliptic Z           -0.15665760 +/-    0.0000
Ecliptic XDOT         0.00279816 +/-    0.0000
Ecliptic YDOT        -0.00170411 +/-    0.0000
Ecliptic ZDOT        -0.00075232 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   35.40918679 +/-    0.0000
Geocenter to KBO     34.39824861 +/-    0.0000
# Hcoef:  6.54

The following table shows the complete astrometric record for 119068. 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 (119068) followed by the observatory code and reference code for the source of the astrometry.

2001 05  23.17570  15 46 14.01   -20 09 22.2   21.5R 119068    807  Cd1817      
2001 05  23.23965  15 46 13.64   -20 09 21.3         119068    807  Cd1817      
2001 06  13.05311  15 44 18.65   -20 04 49.0   21.9R 119068    304  Cd1817      
2001 06  13.17862  15 44 17.95   -20 04 47.2         119068    304  Cd1817      
2001 06  19.23992  15 43 47.78   -20 03 37.1   22.9R 119068    688  Cd1817      
2001 06  19.29580  15 43 47.53   -20 03 35.6         119068    688  Cd1817      
2002 04  06.26872  15 58 08.59   -21 09 27.1   20.7R 119068    807  Cf4617      
2002 04  06.40072  15 58 08.11   -21 09 26.6         119068    807  Cf4617      
2002 04  07.27381  15 58 04.90   -21 09 22.1         119068    807  Cf4617      
2002 07  09.98894  15 50 12.52   -20 53 03.5   21.9R 119068    304  Cf9823      
2002 07  10.13977  15 50 11.99   -20 53 02.6         119068    304  Cf9823      
2002 07  11.99032  15 50 05.88   -20 52 50.3         119068    304  Cf9823      
2002 07  12.00947  15 50 05.81   -20 52 50.2         119068    304  Cf9823      
2002 07  12.97196  15 50 02.75   -20 52 44.0         119068    304  Cf9823      
2002 07  13.02709  15 50 02.57   -20 52 43.7         119068    304  Cf9823      
2003 04  29.54726  16 04 23.66   -21 56 49.5   21.8R 119068    568  Ch9866      
2003 04  29.59778  16 04 23.40   -21 56 49.3         119068    568  Ch9866      
2003 04  30.58622  16 04 18.25   -21 56 40.6         119068    568  Ch9866      
2005 05  10.24161  16 19 37.77   -23 31 34.8   21.2R 119068    807  Cn5310      
2005 05  10.30813  16 19 37.40   -23 31 34.1         119068    807  Cn5310      
2005 05  11.16906  16 19 32.58   -23 31 27.7         119068    807  Cn5310      

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    -0.20       0.00     0.03
     2   0.0002      0.00    -0.13       0.00     0.06
     3   0.0572      0.00     0.50       0.00    -0.29
     4   0.0575      0.00    -0.13       0.00    -0.01
     5   0.0741      0.00     0.13       0.00    -0.14
     6   0.0743      0.00     0.49       0.00     0.74
     7   0.8709      0.00    -0.23       0.00     0.26
     8   0.8713      0.00    -0.03       0.00     0.08
     9   0.8736      0.00    -0.05       0.00     0.04
    10   1.1302      0.00    -0.02       0.00     0.10
    11   1.1306      0.00    -0.06       0.00    -0.04
    12   1.1357      0.00     0.01       0.00     0.01
    13   1.1358      0.00    -0.09       0.00    -0.01
    14   1.1384      0.00    -0.14       0.00     0.17
    15   1.1385      0.00    -0.18       0.00     0.14
    16   1.9339      0.00    -0.08       0.00    -0.45
    17   1.9341      0.00     0.03       0.00    -0.70
    18   1.9368      0.00     0.18       0.00    -0.72
    19   3.9646      0.00    -0.00       0.00     0.16
    20   3.9648      0.00     0.12       0.00     0.35
    21   3.9671      0.00     0.00       0.00     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.

119068    quality flag:3

Type:         5:2EEE    5:2EEE    5:2EEE

axisobj        54.643    54.643    54.643
ecceobj         0.352     0.352     0.352
incobj         12.936    12.936    12.936
qmin           34.877    34.873    34.877
qmax           77.469    77.431    77.481
amean          55.463    55.463    55.463
amin           54.635    54.641    54.620
amax           56.480    56.467    56.483
emean           0.358     0.358     0.358
emin            0.344     0.344     0.344
emax            0.373     0.372     0.373
imean          12.165    12.165    12.164
imin           11.747    11.747    11.746
imax           12.604    12.605    12.608
excite_mean     0.416     0.416     0.416
fracstop        1.000     1.000     1.000
cjmean          3.020     3.020     3.020

libcent 0       180.3     180.3     180.3
libamp  0       145.1     145.0     145.1
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       176.2     176.0     176.3
kozaiamp        179.9     179.9     179.9