Orbit Fit and Astrometric record for 69988

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: 69988     
# Created Sun Nov 22 02:37:00 2009
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting   22 observations of   24
# Arc:   2.18y
# First observation: 1998/10/22
#  Last observation: 2000/12/28
# Chi-squared of fit:   130.60 DOF:   38 RMS:  0.43
# Min/Max residuals:    -1.07    1.00
# Exact a, adot, b, bdot, g, gdot:
  1.900246E-05  2.866703E-02  2.494950E-06  4.561836E-03  2.658501E-02  9.896219E-03
# 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
    2.777858   37.434808    0.144484    0.047158   -0.976638  2451108.840261
# Heliocentric elements and errors
Epoch:              2451110.5000  =  1998/10/24
Mean Anomaly:           27.19484 +/-     0.000
Argument of Peri:      310.52505 +/-     0.000
Long of Asc Node:       20.67179 +/-     0.000
Inclination:             9.43013 +/-     0.000
Eccentricity:         0.43300087 +/-    0.0000
Semi-Major Axis:     55.79596327 +/-    0.0000
Time of Perihelion: 2439610.7970 +/-       0.0
Perihelion:          31.63626262 +/-    0.0000
Aphelion:            79.95566392 +/-    0.0000
Period (y)              416.7853 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           30.70524930 +/-    0.0000
Ecliptic Y           23.31708072 +/-    0.0000
Ecliptic Z            1.82307683 +/-    0.0000
Ecliptic XDOT        -0.00100460 +/-    0.0000
Ecliptic YDOT         0.00295826 +/-    0.0000
Ecliptic ZDOT         0.00051860 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   38.59799575 +/-    0.0000
Geocenter to KBO     37.61499794 +/-    0.0000
# Hcoef:  7.48

The following table shows the complete astrometric record for 69988. 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 (69988) followed by the observatory code and reference code for the source of the astrometry.

1998 10  22.33953  02 16 33.37   +16 37 01.2   23.4R 69988     695  Ch1098      
1998 10  22.47242  02 16 32.66   +16 36 58.0         69988     695  Ch1098      
1998 10  22.49896  02 16 32.59   +16 36 57.5         69988     695  Ch1098      
1998 11  18.08751  02 14 16.22   +16 26 29.7   22.8R 69988     695  Ca3373      
1998 11  18.15650  02 14 15.84   +16 26 27.9         69988     695  Ca3373      
1998 11  18.24171  02 14 15.42   +16 26 26.1         69988     695  Ca3373      
1998 11  19.07963  02 14 11.38   +16 26 06.3   22.5R 69988     695  Ca3373      
1998 11  19.16041  02 14 11.00   +16 26 04.5         69988     695  Ca3373      
1998 12  17.83243  02 12 16.71   +16 16 23.3         69988     950  Ca3608      
1998 12  17.86950  02 12 16.68   +16 16 21.8         69988     950  Ca3608      
1998 12  17.90432  02 12 16.56   +16 16 20.2         69988     950  Ca3608      
2000 01  06.29250  02 17 37.46   +16 59 04.4         69988     568  Cc9443      
2000 01  06.32548  02 17 37.41   +16 59 03.8         69988     568  Cc9443      
2000 01  07.28238  02 17 36.24   +16 58 56.0         69988     568  Cc9443      
2000 01  07.31050  02 17 36.21   +16 58 55.5         69988     568  Cc9443      
2000 02  05.09634  02 17 45.90   +16 58 31.3   23.2R 69988     695  Cj9811      
2000 02  05.10277  02 17 45.86   +16 58 32.5         69988     695  Cj9811      
2000 02  05.19148  02 17 46.01   +16 58 33.1         69988     695  Cj9811      
2000 12  24.23678  02 23 58.83   +17 46 36.3         69988     568  Cc9443      
2000 12  24.34670  02 23 58.51   +17 46 34.6         69988     568  Cc9443      
2000 12  28.28859  02 23 49.021  +17 45 40.44  23.3R 69988     568  Cl8213      
2000 12  28.35747  02 23 48.856  +17 45 39.61  23.2R 69988     568  Cl8213      
2003 10  22.31297  02 46 20.85   +20 14 21.3   23.3R 69988     304  Ci9217      
2003 10  22.32738  02 46 20.79   +20 14 20.3         69988     304  Ci9217      

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    -0.21       0.00    -0.75
  2   0.0004      0.00    -0.54       0.00    -0.24
  3   0.0004      0.00     0.49       0.00    -0.14
  4   0.0732      0.00     0.84       0.00     0.23
  5   0.0734      0.00     0.22       0.00     0.03
  6   0.0737      0.00     0.22       0.00     0.22
  7   0.0759      0.00     0.13       0.00     0.04
  8   0.0762      0.00     0.33       0.00     0.11
  9   0.1547      0.00    -1.07       0.00     1.00
 10   0.1548      0.00     0.17       0.00     0.09
 11   0.1549      0.00    -0.05       0.00    -0.96
 12   1.2073      0.00    -0.22       0.00     0.18
 13   1.2074      0.00    -0.30       0.00    -0.13
 14   1.2100      0.00    -0.37       0.00     0.04
 15   1.2101      0.00    -0.29       0.00    -0.22
 16   1.2889      0.00     0.99       0.00    -0.85
 17   1.2889      0.00     0.22       0.00     0.31
 18   1.2891      0.00     0.09       0.00     0.33
 19   2.1736      0.00     0.16       0.00    -0.09
 20   2.1739      0.00    -0.21       0.00    -0.18
 21   2.1847      0.00     0.04       0.00     0.19
 22   2.1849      0.00    -0.04       0.00     0.26
 23   4.9992      0.00 ( -11.54)      0.00 (   2.68)
 24   4.9993      0.00 ( -11.35)      0.00 (   1.94)

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.

69988    quality flag:3

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

axisobj        55.801    55.801    55.800
ecceobj         0.432     0.432     0.432
incobj          9.432     9.432     9.432
qmin           31.054    31.045    31.047
qmax           81.651    81.669    81.591
amean          55.463    55.463    55.463
amin           54.553    54.593    54.570
amax           56.619    56.650    56.616
emean           0.430     0.430     0.430
emin            0.418     0.418     0.418
emax            0.442     0.442     0.442
imean           9.426     9.444     9.440
imin            9.109     9.102     9.109
imax            9.807     9.806     9.802
excite_mean     0.460     0.460     0.460
fracstop        1.000     1.000     1.000
cjmean          2.961     2.961     2.961

libcent 0       181.6     179.7     179.8
libamp  0       141.5     138.5     141.4
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       172.5     175.7     173.1
kozaiamp        180.0     180.0     180.0