Orbit Fit and Astrometric record for 84522

The following information shows the result of the orbit fit based on Gary Bernstein's method. Most of the information should be self-explanatory.

# Object: 84522     
# Created Fri May  2 02:36:19 2008
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting   55 observations of   55
# Arc:   7.11y
# First observation: 2000/08/05
#  Last observation: 2007/09/16
# Chi-squared of fit:   457.08 DOF:  104 RMS:  0.51
# Min/Max residuals:    -1.97    1.23
# Exact a, adot, b, bdot, g, gdot:
  9.006279E-06  1.551770E-02  1.174240E-05  1.077557E-02  2.057120E-02 -4.997399E-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
    1.940581   27.756363    0.977607    0.008862   -0.267119  2451762.086893
# Heliocentric elements and errors
Epoch:              2451760.5000  =  2000/08/04
Mean Anomaly:          310.18507 +/-     0.000
Argument of Peri:       85.46097 +/-     0.000
Long of Asc Node:       23.84689 +/-     0.000
Inclination:            34.93667 +/-     0.000
Eccentricity:         0.29745002 +/-    0.0000
Semi-Major Axis:     55.83752160 +/-    0.0000
Time of Perihelion: 2472848.9493 +/-       0.0
Perihelion:          39.22864983 +/-    0.0000
Aphelion:            72.44639337 +/-    0.0000
Period (y)              417.2510 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           43.69087836 +/-    0.0000
Ecliptic Y           21.89002974 +/-    0.0000
Ecliptic Z            1.64671910 +/-    0.0000
Ecliptic XDOT        -0.00160021 +/-    0.0000
Ecliptic YDOT         0.00150097 +/-    0.0000
Ecliptic ZDOT         0.00141094 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   48.89578091 +/-    0.0000
Geocenter to KBO     48.61187719 +/-    0.0000
# Hcoef:  3.85

The following table shows the complete astrometric record for 84522. 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 (84522) followed by the observatory code and reference code for the source of the astrometry.

2000 08  05.58615  01 40 14.71   +12 29 12.0         84522     608  Cg8140      
2001 08  05.49000  01 42 46.04   +13 23 15.5   20.7R 84522     644  Cg8140      
2001 10  07.38997  01 39 46.60   +13 15 52.6         84522     644  Cg8140      
2001 10  19.36607  01 38 54.82   +13 12 25.9   20.8R 84522     644  Cg8140      
2001 10  26.30785  01 38 24.60   +13 10 19.9         84522     644  Cg8140      
2002 10  09.21525  01 42 14.08   +14 10 55.7   20.4  84522     644  Cg6278      
2002 10  09.29517  01 42 13.71   +14 10 54.6         84522     644  Cg6278      
2002 10  09.35802  01 42 13.44   +14 10 53.5         84522     644  Cg6278      
2002 10  31.29667  01 40 37.47   +14 04 25.5         84522     608  Cg8140      
2002 11  03.10860  01 40 25.42   +14 03 33.3   20.4  84522     644  Cg6278      
2002 11  03.17245  01 40 25.10   +14 03 32.1         84522     644  Cg6278      
2002 11  06.92556  01 40 09.26   +14 02 22.9   20.2R 84522     966  Cg6278      
2002 11  07.01253  01 40 08.88   +14 02 20.8   20.4R 84522     966  Cg6278      
2002 11  07.04701  01 40 08.64   +14 02 21.1   19.7R 84522     246  Cg6278      
2002 11  07.05161  01 40 08.59   +14 02 21.1         84522     246  Cg6278      
2002 11  07.05242  01 40 08.57   +14 02 20.7         84522     246  Cg6278      
2002 11  07.17275  01 40 08.22   +14 02 18.6   20.5R 84522     649  Cg6278      
2002 11  07.26611  01 40 07.83   +14 02 17.4         84522     926  Cg6278      
2002 11  07.32098  01 40 07.58   +14 02 15.5   20.5R 84522     649  Cg6278      
2002 11  07.33484  01 40 07.54   +14 02 16.4   19.2R 84522     926  Cg6278      
2002 11  08.83631  01 40 01.22   +14 01 49.0         84522     587  Cg6278      
2002 11  08.91919  01 40 00.97   +14 01 47.4         84522     587  Cg6278      
2002 11  10.80016  01 39 53.27   +14 01 12.7         84522     246  Cg6279      
2002 11  10.80284  01 39 53.25   +14 01 13.3         84522     246  Cg6279      
2002 11  12.24598  01 39 47.41   +14 00 48.6   20.2R 84522     644  Cg8140      
2002 11  22.22356  01 39 09.12   +13 57 57.4   21.   84522     644  Ci9417      
2002 12   5.12153  01 38 26.865  +13 54 46.79  20.5R 84522     662              
2002 12   5.21266  01 38 26.590  +13 54 45.43        84522     662              
2002 12  08.87733  01 38 16.43   +13 53 58.8   20.1R 84522     621  Cg8140      
2002 12  08.88885  01 38 16.37   +13 53 59.3   20.4R 84522     621  Cg8140      
2002 12  08.90038  01 38 16.35   +13 53 58.7   20.7R 84522     621  Cg8140      
2002 12  08.91578  01 38 16.30   +13 53 58.4   20.3R 84522     621  Cg8140      
2002 12  09.88776  01 38 13.80   +13 53 48.1   20.1R 84522     540  Cg8140      
2002 12  10.90954  01 38 11.21   +13 53 35.4   20.3R 84522     540  Cg8140      
2002 12  10.92207  01 38 11.12   +13 53 35.9   20.3R 84522     621  Cg8140      
2002 12  10.93728  01 38 11.06   +13 53 35.6   20.8R 84522     621  Cg8140      
2002 12  11.08333  01 38 10.69   +13 53 33.2   21.4R 84522     926  Cg8140      
2002 12  11.15628  01 38 10.53   +13 53 33.4   21.3R 84522     926  Cg8140      
2002 12  11.23378  01 38 10.29   +13 53 31.8   21.2R 84522     926  Cg8140      
2003 07  06.58329  01 47 42.37   +15 05 33.3   20.2R 84522     568  Ci2694      
2003 07  07.58629  01 47 43.91   +15 05 54.0         84522     568  Ci2694      
2003 10  17.21268  01 44 16.86   +15 04 42.8   21.1V 84522     691  Ck3845      
2003 10  17.24942  01 44 16.67   +15 04 42.5   21.1V 84522     691  Ck3845      
2003 10  17.27854  01 44 16.54   +15 04 41.7   21.3V 84522     691  Ck3845      
2003 12  17.84368  01 40 28.52   +14 48 00.2   20.5R 84522     621  Cj4691      
2003 12  17.86701  01 40 28.44   +14 48 00.3         84522     621  Cj4691      
2003 12  17.89035  01 40 28.43   +14 47 59.6         84522     621  Cj4691      
2003 12  18.77428  01 40 26.62   +14 47 51.2   20.3R 84522     621  Cj4691      
2003 12  18.80927  01 40 26.51   +14 47 50.6         84522     621  Cj4691      
2006 11  16.88427  01 50 06.07   +17 46 02.4         84522     540  Cs8083      
2006 11  16.94563  01 50 05.71   +17 46 00.1   20.5V 84522     540  Cs8083      
2006 11  20.78460  01 49 50.30   +17 44 49.8         84522     540  Ct0042      
2006 11  20.87538  01 49 49.91   +17 44 47.7   20.5V 84522     540  Ct0042      
2007 09  16.40182  01 57 22.35   +18 59 03.5   20.3R 84522     675  Cy7378      
2007 09  16.46046  01 57 22.14   +18 59 03.1   20.4R 84522     675  Cy7378      

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    -0.15       0.00    -0.24
  2   0.9991      0.00    -0.65       0.00    -0.45
  3   1.1713      0.00     0.42       0.00    -0.60
  4   1.2041      0.00     0.10       0.00    -0.13
  5   1.2231      0.00     0.09       0.00    -0.11
  6   2.1756      0.00     0.29       0.00     0.20
  7   2.1758      0.00    -0.04       0.00     0.40
  8   2.1760      0.00     0.04       0.00     0.33
  9   2.2360      0.00    -0.22       0.00     0.73
 10   2.2437      0.00     0.34       0.00     0.25
 11   2.2439      0.00    -0.33       0.00     0.21
 12   2.2542      0.00     0.30       0.00    -0.33
 13   2.2544      0.00     0.12       0.00    -0.85
 14   2.2545      0.00    -1.26       0.00     0.08
 15   2.2545      0.00    -1.72       0.00     0.16
 16   2.2545      0.00    -1.97       0.00    -0.23
 17   2.2549      0.00     0.19       0.00    -0.18
 18   2.2551      0.00     0.24       0.00     0.30
 19   2.2553      0.00     0.01       0.00    -0.58
 20   2.2553      0.00     0.26       0.00     0.55
 21   2.2594      0.00    -1.15       0.00     0.38
 22   2.2596      0.00     0.30       0.00     0.27
 23   2.2648      0.00     0.42       0.00    -0.62
 24   2.2648      0.00     0.28       0.00     0.03
 25   2.2687      0.00     0.36       0.00     0.98
 26   2.2961      0.00    -0.63       0.00    -0.06
 27   2.3314      0.00    -0.11       0.00     0.35
 28   2.3316      0.00    -0.18       0.00     0.19
 29   2.3417      0.00     0.41       0.00    -0.33
 30   2.3417      0.00    -0.02       0.00     0.31
 31   2.3417      0.00     0.14       0.00    -0.15
 32   2.3418      0.00     0.02       0.00    -0.27
 33   2.3444      0.00     0.83       0.00     0.93
 34   2.3472      0.00     1.23       0.00    -0.01
 35   2.3473      0.00     0.35       0.00     0.64
 36   2.3473      0.00     0.03       0.00     0.51
 37   2.3477      0.00    -0.15       0.00    -0.29
 38   2.3479      0.00     0.27       0.00     0.72
 39   2.3481      0.00    -0.34       0.00     0.00
 40   2.9158      0.00     0.72       0.00    -0.60
 41   2.9185      0.00     0.02       0.00    -0.11
 42   3.1968      0.00     0.39       0.00     0.00
 43   3.1969      0.00     0.02       0.00     0.33
 44   3.1970      0.00     0.03       0.00     0.03
 45   3.3655      0.00     0.24       0.00    -0.29
 46   3.3656      0.00    -0.21       0.00     0.04
 47   3.3657      0.00     0.40       0.00    -0.42
 48   3.3681      0.00     0.83       0.00    -0.16
 49   3.3682      0.00     0.28       0.00    -0.42
 50   6.2814      0.00     0.14       0.00     0.18
 51   6.2816      0.00    -1.41       0.00    -0.96
 52   6.2921      0.00     0.42       0.00     0.26
 53   6.2924      0.00     0.04       0.00    -0.17
 54   7.1124      0.00     0.37       0.00     0.26
 55   7.1126      0.00     0.39       0.00     0.19

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.

84522    quality flag:3

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

axisobj       55.835    55.834    55.835
ecceobj        0.297     0.297     0.297
incobj        34.923    34.923    34.923
qmin          30.312    30.311    30.281
qmax          82.089    82.110    81.986
amean         55.461    55.461    55.461
amin          54.715    54.707    54.719
amax          56.423    56.434    56.412
emean          0.386     0.386     0.385
emin           0.285     0.285     0.285
emax           0.455     0.455     0.455
imean         31.541    31.536    31.549
imin          28.562    28.572    28.553
imax          35.025    35.025    35.025
fracstop       1.000     1.000     1.000
cjmean         2.672     2.672     2.672

libcent 0      183.1     183.3     183.0
libamp  0      134.0     134.1     133.8
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      127.7     128.1     127.0
kozaiamp        45.2      45.5      44.5