Orbit Fit and Astrometric record for 04TZ387

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: 04TZ387   
# Created Fri Nov 22 02:08:42 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     50 observations of     51
# Arc:   8.16y
# First observation: 2004/10/13
#  Last observation: 2012/12/12
# Chi-squared of fit:   256.05 DOF:     94 RMS:  0.40
# Min/Max residuals:    -0.76    1.24
# Exact a, adot, b, bdot, g, gdot:
  5.108980E-05  1.576921E+00  2.568509E-06  2.363138E-02  4.445439E-01  7.576753E-01
# Covariance matrix:
  2.2412E-09 -5.9707E-06  5.1629E-11 -1.3651E-07  1.1769E-09 -6.7946E-06
 -5.9707E-06  1.6060E-02 -1.3759E-07  3.6716E-04 -3.1313E-06  1.8276E-02
  5.1629E-11 -1.3759E-07  1.9550E-12 -3.1769E-09  2.7120E-11 -1.5658E-07
 -1.3651E-07  3.6716E-04 -3.1769E-09  8.9890E-06 -7.1592E-08  4.1784E-04
  1.1769E-09 -3.1313E-06  2.7120E-11 -7.1592E-08  6.1835E-10 -3.5634E-06
 -6.7946E-06  1.8276E-02 -1.5658E-07  4.1784E-04 -3.5634E-06  2.0798E-02
#      lat0       lon0       xBary       yBary       zBary        JD0
    1.477326   56.504465    0.592646    0.020900   -0.806757  2453291.911113
# Heliocentric elements and errors
Epoch:              2453291.5000  =  2004/10/13
Mean Anomaly:           34.22452 +/-     0.002
Argument of Peri:      337.25968 +/-     0.000
Long of Asc Node:        3.49545 +/-     0.000
Inclination:             1.59326 +/-     0.000
Eccentricity:         0.33118046 +/-    0.0533
Semi-Major Axis:      3.98588185 +/-    0.0000
Time of Perihelion: 2453015.1752 +/-       0.0
Perihelion:           2.66583566 +/-    0.2123
Aphelion:             5.30592804 +/-    0.2123
Period (y)                7.9578 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X            2.17631158 +/-    0.0000
Ecliptic Y            2.22217093 +/-    0.0000
Ecliptic Z            0.05800359 +/-    0.0000
Ecliptic XDOT        -0.00552818 +/-    0.0000
Ecliptic YDOT         0.00923960 +/-    0.0000
Ecliptic ZDOT         0.00026589 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO    3.11087311 +/-    0.0000
Geocenter to KBO      2.24947392 +/-    0.0000
# Hcoef: 15.77

The following table shows the complete astrometric record for 04TZ387. 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 (04TZ387) followed by the observatory code and reference code for the source of the astrometry.

2004 10  13.41037  03 35 19.11   +20 48 34.1   20.6V 04TZ387   691  C~5VAB      
2004 10  13.43812  03 35 18.25   +20 48 32.7   20.7V 04TZ387   691  C~5VAB      
2004 10  13.46492  03 35 17.45   +20 48 31.0   20.6V 04TZ387   691  C~5VAB      
2004 10  23.27514  03 29 44.76   +20 35 11.0   20.8V 04TZ387   691  C~5VAB      
2004 10  23.30384  03 29 43.59   +20 35 08.5   20.2V 04TZ387   691  C~5VAB      
2004 10  23.34398  03 29 42.00   +20 35 04.1   20.3V 04TZ387   691  C~5VAB      
2010 05  18.40361  14 58 18.49   -18 31 57.5   21.4r 04TZ387   F51  C~7APo      
2010 05  18.41442  14 58 18.03   -18 31 55.6   21.6r 04TZ387   F51  C~7APo      
2011 07  21.50169  20 27 43.02   -21 22 23.3   18.9z 04TZ387   F51  C~7APo      
2011 07  27.43565  20 23 27.075  -21 35 32.73  20.3g 04TZ387   F51  C~5VAB      
2011 07  27.44530  20 23 26.634  -21 35 33.79  20.2g 04TZ387   F51  C~5VAB      
2011 07  27.45569  20 23 26.159  -21 35 35.18  19.6r 04TZ387   F51  C~5VAB      
2011 07  27.46498  20 23 25.729  -21 35 36.32  19.6r 04TZ387   F51  C~5VAB      
2011 07  27.64891  20 23 17.62   -21 35 56.0   19.2V 04TZ387   E12  C~5VAB      
2011 07  27.66103  20 23 17.08   -21 35 57.4   19.8V 04TZ387   E12  C~5VAB      
2011 07  27.67311  20 23 16.51   -21 35 58.8   19.5V 04TZ387   E12  C~5VAB      
2011 08  15.37262  20 10 27.83   -22 07 49.8         04TZ387   F51  C~7APo      
2011 08  15.38390  20 10 27.40   -22 07 50.6   19.2y 04TZ387   F51  C~7APo      
2011 09  14.30135  20 02 17.30   -22 07 35.3   19.6y 04TZ387   F51  C~7APo      
2011 10  18.24103  20 19 29.96   -20 45 54.3   20.8r 04TZ387   F51  C~7APo      
2011 10  18.25242  20 19 30.53   -20 45 52.0   20.9r 04TZ387   F51  C~7APo      
2011 10  21.21351  20 22 11.45   -20 34 44.3   20.4z 04TZ387   F51  C~7APo      
2011 11  16.20928  20 51 41.730  -18 28 29.21  21.3w 04TZ387   F51  C~5VAB      
2011 11  16.21907  20 51 42.489  -18 28 25.70  21.2w 04TZ387   F51  C~5VAB      
2011 11  16.22395  20 51 42.859  -18 28 23.99  21.3w 04TZ387   F51  C~5VAB      
2012 10  14.41178  03 58 56.24   +22 07 54.3   20.9V 04TZ387   691  C~5VAB      
2012 10  14.41425  03 58 56.17   +22 07 54.9   20.8V 04TZ387   691  C~5VAB      
2012 10  14.42954  03 58 55.81   +22 07 54.1   21.1V 04TZ387   691  C~5VAB      
2012 10  14.43201  03 58 55.73   +22 07 54.1   20.9V 04TZ387   691  C~5VAB      
2012 10  14.44724  03 58 55.35   +22 07 53.1   20.8V 04TZ387   691  C~5VAB      
2012 10  14.44972  03 58 55.28   +22 07 53.5   20.8V 04TZ387   691  C~5VAB      
2012 10  22.43438  03 55 02.25   +22 01 30.6   20.7V 04TZ387   691  C~5VAB      
2012 10  22.45208  03 55 01.63   +22 01 29.3   20.6V 04TZ387   691  C~5VAB      
2012 10  22.46978  03 55 00.97   +22 01 28.2   20.5V 04TZ387   691  C~5VAB      
2012 10  24.59705  03 53 46.64   +21 59 01.5   20.4r 04TZ387   F51  C~7APo      
2012 10  24.60112  03 53 46.50   +21 59 01.3   20.3r 04TZ387   F51  C~7APo      
2012 10  24.61487  03 53 45.97   +21 59 00.3   20.5r 04TZ387   F51  C~7APo      
2012 11  05.20528  03 45 51.14   +21 40 26.5   20.9V 04TZ387   691  C~5VAB      
2012 11  05.22645  03 45 50.17   +21 40 24.4   20.6V 04TZ387   691  C~5VAB      
2012 11  05.24415  03 45 49.37   +21 40 23.3   20.4V 04TZ387   691  C~5VAB      
2012 11  05.37615  03 45 43.41   +21 40 07.7   20.3i 04TZ387   F51  C~7APo      
2012 11  05.38923  03 45 42.80   +21 40 06.2   20.2i 04TZ387   F51  C~7APo      
2012 11  06.53086  03 44 50.75   +21 37 50.3   20.2i 04TZ387   F51  C~7APo      
2012 11  06.54400  03 44 50.13   +21 37 48.5   20.2i 04TZ387   F51  C~7APo      
2012 11  17.15871  03 36 29.82   +21 13 54.1         04TZ387   691  C~5ZVY      
2012 11  17.17405  03 36 29.06   +21 13 52.7         04TZ387   691  C~5ZVY      
2012 11  17.18938  03 36 28.10   +21 13 50.9         04TZ387   691  C~5ZVY      
2012 12  07.416950 03 21 51.40   +20 23 45.3   19.0J 04TZ387   T11  C~7xJC      
2012 12  12.11037  03 19 12.63   +20 13 21.8   20.6V 04TZ387   691  C~5VAB      
2012 12  12.17347  03 19 10.61   +20 13 14.2   20.7V 04TZ387   691  C~5VAB      
2012 12  12.22120  03 19 09.08   +20 13 08.1   20.8V 04TZ387   691  C~5VAB      

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     1.15       0.00    -0.11
     2   0.0001      0.00     0.73       0.00     0.16
     3   0.0001      0.00     0.76       0.00     0.10
     4   0.0270      0.00     1.14       0.00     0.25
     5   0.0271      0.00     0.85       0.00     0.61
     6   0.0272      0.00     1.24       0.00     0.29
     7   5.5934      0.00     0.79       0.00     0.33
     8   5.5934      0.00     0.75       0.00     0.44
     9   6.7682      0.00     0.56       0.00     0.27
    10   6.7845      0.00     1.02       0.00     0.12
    11   6.7845      0.00     1.05       0.00     0.30
    12   6.7845      0.00     1.07       0.00     0.24
    13   6.7845      0.00     1.01       0.00     0.29
    14   6.7850      0.00     0.97       0.00     0.08
    15   6.7851      0.00     1.15       0.00     0.19
    16   6.7851      0.00     0.84       0.00     0.28
    17   6.8363      0.00     1.06       0.00     0.27
    18   6.8363      0.00     0.93       0.00     0.23
    19   6.9183      0.00     0.58       0.00     0.29
    20   7.0112      0.00     0.51       0.00     0.28
    21   7.0112      0.00     0.32       0.00     0.07
    22   7.0193      0.00     0.47       0.00     0.08
    23   7.0905      0.00     0.74       0.00     0.02
    24   7.0905      0.00     0.80       0.00     0.07
    25   7.0905      0.00     0.70       0.00     0.06
    26   8.0027      0.00    -0.25       0.00    -0.19
    27   8.0027      0.00    -0.35       0.00     0.49
    28   8.0028      0.00     0.14       0.00     0.17
    29   8.0028      0.00    -0.11       0.00     0.25
    30   8.0028      0.00     0.05       0.00    -0.26
    31   8.0028      0.00    -0.04       0.00     0.22
    32   8.0247      0.00     0.17       0.00     0.12
    33   8.0248      0.00     0.21       0.00     0.01
    34   8.0248      0.00    -0.35       0.00     0.12
    35   8.0306      0.00     0.30       0.00     0.01
    36   8.0306      0.00     0.48       0.00     0.13
    37   8.0307      0.00     0.23       0.00     0.21
    38   8.0624      0.00     0.01       0.00    -0.20
    39   8.0625      0.00     0.09       0.00     0.06
    40   8.0625      0.00     0.36       0.00     0.94
    41   8.0629      0.00     0.17       0.00     0.02
    42   8.0629      0.00     0.15       0.00     0.00
    43   8.0660      0.00     0.34       0.00     0.13
    44   8.0661      0.00     0.34       0.00    -0.03
    45   8.0951      0.00     0.40       0.00    -0.55
    46   8.0952      0.00     0.18       0.00     0.20
    47   8.0952      0.00 (  -3.02)      0.00 (   0.56)
    48   8.1506      0.00     0.76       0.00     0.27
    49   8.1634      0.00    -0.76       0.00     0.04
    50   8.1636      0.00    -0.24       0.00     0.19
    51   8.1638      0.00     0.20       0.00     0.05

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.

04TZ387    quality flag:3

Type:       CENTAURR  CENTAURR  CENTAURR

axisobj         3.980     3.980     3.980
ecceobj         0.332     0.332     0.332
incobj          1.596     1.596     1.596
qmin            2.656     2.656     2.656
qmax            5.303     5.303     5.303
amean           3.980     3.980     3.980
amin            3.980     3.980     3.980
amax            3.980     3.980     3.980
emean           0.332     0.332     0.332
emin            0.332     0.332     0.332
emax            0.332     0.332     0.332
imean           2.504     2.504     2.504
imin            2.504     2.504     2.504
imax            2.504     2.504     2.504
excite_mean     0.335     0.335     0.335
fracstop        0.000     0.000     0.000
cjmean          8.249     8.249     8.249

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       337.5     337.5     337.5
kozaiamp          0.0       0.0       0.0