Orbit Fit and Astrometric record for 03TJ58

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: 03TJ58    
# Created Sat Jun  6 01:09:09 2020
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting   52 observations of   52
# Arc:  16.29y
# First observation: 2003/10/03
#  Last observation: 2020/01/18
# Chi-squared of fit:   206.16 DOF:   98 RMS:  0.35
# Min/Max residuals:    -0.73    0.64
# Exact a, adot, b, bdot, g, gdot:
  1.656660E-05  2.532169E-02  1.576177E-07  3.435670E-04  2.478313E-02  1.328291E-03
# Covariance matrix:
  2.3480E-13 -6.1700E-14  1.2981E-15 -7.8739E-16  1.0279E-13 -1.2609E-13
 -6.1700E-14  2.3326E-14 -5.9097E-16  3.1238E-16 -1.5243E-14  5.0225E-14
  1.2981E-15 -5.9097E-16  5.2573E-14 -5.9966E-15  8.5681E-17 -1.3648E-15
 -7.8739E-16  3.1238E-16 -5.9966E-15  1.4409E-15 -2.0544E-16  7.1706E-16
  1.0279E-13 -1.5243E-14  8.5681E-17 -2.0544E-16  1.1187E-13 -3.2231E-14
 -1.2609E-13  5.0225E-14 -1.3648E-15  7.1706E-16 -3.2231E-14  1.1531E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
    0.544431   72.790778    0.895546    0.004332   -0.451854  2452915.960933
# Heliocentric elements and errors
Epoch:              2452916.5000  =  2003/10/04
Mean Anomaly:           16.67339 +/-     0.008
Argument of Peri:       14.24028 +/-     0.010
Long of Asc Node:       37.36361 +/-     0.003
Inclination:             0.95814 +/-     0.000
Eccentricity:         0.08892447 +/-    0.0000
Semi-Major Axis:     44.57824947 +/-    0.0030
Time of Perihelion: 2447881.4443 +/-       2.4
Perihelion:          40.61415240 +/-    0.0035
Aphelion:            48.54234655 +/-    0.0040
Period (y)              297.6410 +/-      0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           12.92298224 +/-    0.0002
Ecliptic Y           38.71212426 +/-    0.0005
Ecliptic Z            0.38341917 +/-    0.0000
Ecliptic XDOT        -0.00263371 +/-    0.0000
Ecliptic YDOT         0.00096150 +/-    0.0000
Ecliptic ZDOT         0.00003951 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   40.81393827 +/-    0.0005
Geocenter to KBO     40.35001554 +/-    0.0005
# Hcoef:  7.60

The following table shows the complete astrometric record for 03TJ58. 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 (03TJ58) followed by the observatory code and reference code for the source of the astrometry.

2003 10  03.46019  04 45 05.02   +22 52 18.3   23.0i 03TJ58    568  Cq9898      
2003 10  03.51093  04 45 04.92   +22 52 18.1   23.7i 03TJ58    568  Cq9898      
2003 10  03.57232  04 45 04.79   +22 52 18.0   23.1i 03TJ58    568  Cq9898      
2003 12  16.32636  04 39 40.38   +22 42 59.8   23.5g 03TJ58    568  Cq9898      
2003 12  16.35282  04 39 40.24   +22 42 59.4   23.5g 03TJ58    568  Cq9898      
2003 12  16.37913  04 39 40.10   +22 42 59.1   23.6g 03TJ58    568  Cq9898      
2003 12  17.43092  04 39 34.53   +22 42 48.3         03TJ58    568  Cq9898      
2003 12  21.199252 04 39 15.00   +22 42 10.2   22.9V 03TJ58    645  C~2Jx9      
2003 12  21.200082 04 39 15.00   +22 42 10.2   22.7V 03TJ58    645  C~2Jx9      
2003 12  21.202570 04 39 15.02   +22 42 10.1   23.1V 03TJ58    645  C~2Jx9      
2005 12  04.36834  04 53 20.01   +23 09 13.4   23.5r 03TJ58    697  Cq9898      
2005 12  04.39627  04 53 19.83   +23 09 13.0   23.6r 03TJ58    697  Cq9898      
2005 12  04.43534  04 53 19.63   +23 09 12.9   23.4r 03TJ58    697  Cq9898      
2005 12  06.36627  04 53 09.07   +23 08 56.4   23.5r 03TJ58    697  Cq9898      
2005 12  24.27338  04 51 33.26   +23 06 23.7   23.9r 03TJ58    568  C~0D33      
2005 12  24.37142  04 51 32.74   +23 06 22.8   24.3r 03TJ58    568  C~0D33      
2005 12  24.40571  04 51 32.56   +23 06 22.5   24.3r 03TJ58    568  C~0D33      
2005 12  25.40936  04 51 27.43   +23 06 14.1   24.1r 03TJ58    568  C~0D33      
2006 01  28.27637  04 49 09.54   +23 02 13.0         03TJ58    675  Cq9898      
2006 01  29.14157  04 49 07.19   +23 02 08.9         03TJ58    675  Cq9898      
2006 11  22.22759  05 00 45.54   +23 21 24.9   23.1R 03TJ58    250  S~06Ae      
2006 11  22.24361  05 00 45.45   +23 21 24.8         03TJ58    250  S~06Ae      
2006 11  22.24801  05 00 45.43   +23 21 24.8         03TJ58    250  S~06Ae      
2006 11  22.25241  05 00 45.41   +23 21 24.8         03TJ58    250  S~06Ae      
2007 09  03.04753  05 09 54.72   +23 33 12.0   23.4R 03TJ58    250  S~06Ae      
2007 09  03.05448  05 09 54.73   +23 33 12.0         03TJ58    250  S~06Ae      
2007 09  03.06212  05 09 54.75   +23 33 12.0         03TJ58    250  S~06Ae      
2007 09  03.10934  05 09 54.83   +23 33 12.2         03TJ58    250  S~06Ae      
2007 09  03.11837  05 09 54.85   +23 33 12.2         03TJ58    250  S~06Ae      
2007 09  03.12740  05 09 54.87   +23 33 12.2         03TJ58    250  S~06Ae      
2007 09  03.18295  05 09 54.97   +23 33 12.4         03TJ58    250  S~06Ae      
2007 10  22.65934  05 09 17.28   +23 33 18.1         03TJ58    250  S~06Ae      
2007 10  22.66559  05 09 17.26   +23 33 18.1         03TJ58    250  S~06Ae      
2007 10  22.67323  05 09 17.23   +23 33 18.1         03TJ58    250  S~06Ae      
2007 10  22.68226  05 09 17.20   +23 33 18.1         03TJ58    250  S~06Ae      
2007 10  22.72462  05 09 17.07   +23 33 17.9         03TJ58    250  S~06Ae      
2007 10  22.73365  05 09 17.03   +23 33 17.9         03TJ58    250  S~06Ae      
2007 10  22.74129  05 09 17.02   +23 33 17.9         03TJ58    250  S~06Ae      
2007 10  22.74754  05 09 17.00   +23 33 17.8         03TJ58    250  S~06Ae      
2007 11  20.11559  05 07 16.47   +23 31 10.6         03TJ58    250  S~06Ae      
2007 11  20.15865  05 07 16.28   +23 31 11.3         03TJ58    250  S~06Ae      
2007 11  20.16629  05 07 16.23   +23 31 11.3         03TJ58    250  S~06Ae      
2007 11  20.22670  05 07 15.92   +23 31 10.9         03TJ58    250  S~06Ae      
2007 11  20.29337  05 07 15.56   +23 31 09.6         03TJ58    250  S~06Ae      
2007 11  20.30240  05 07 15.52   +23 31 09.5         03TJ58    250  S~06Ae      
2007 11  20.35865  05 07 15.26   +23 31 10.1         03TJ58    250  S~06Ae      
2007 11  20.36490  05 07 15.23   +23 31 10.1         03TJ58    250  S~06Ae      
2019 10  26.375010 06 23 54.36   +24 08 10.5   22.8G 03TJ58    705  C~3cWV      
2019 10  26.427800 06 23 54.26   +24 08 10.6   23.6G 03TJ58    705  C~3cWV      
2019 10  26.488560 06 23 54.13   +24 08 10.7   23.6G 03TJ58    705  C~3cWV      
2020 01  18.313630 06 17 34.928  +24 12 00.13        03TJ58    G37  C~3iHi      
2020 01  18.345780 06 17 34.749  +24 12 00.12        03TJ58    G37  C~3iHi      

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    -0.09       0.00     0.00
  2   0.0001      0.00    -0.06       0.00    -0.09
  3   0.0003      0.00    -0.14       0.00    -0.04
  4   0.2022      0.00    -0.22       0.00     0.34
  5   0.2023      0.00    -0.19       0.00     0.20
  6   0.2024      0.00    -0.17       0.00     0.17
  7   0.2053      0.00    -0.57       0.00    -0.06
  8   0.2156      0.00     0.01       0.00    -0.49
  9   0.2156      0.00     0.08       0.00    -0.48
 10   0.2156      0.00     0.57       0.00    -0.56
 11   2.1709      0.00     0.32       0.00     0.04
 12   2.1709      0.00    -0.06       0.00    -0.11
 13   2.1710      0.00     0.18       0.00     0.13
 14   2.1763      0.00    -0.05       0.00    -0.06
 15   2.2254      0.00     0.26       0.00     0.45
 16   2.2256      0.00     0.14       0.00     0.36
 17   2.2257      0.00     0.12       0.00     0.35
 18   2.2285      0.00     0.09       0.00     0.42
 19   2.3212      0.00     0.09       0.00    -0.15
 20   2.3236      0.00    -0.15       0.00     0.17
 21   3.1369      0.00     0.48       0.00     0.05
 22   3.1370      0.00     0.38       0.00     0.06
 23   3.1370      0.00     0.43       0.00     0.09
 24   3.1370      0.00     0.47       0.00     0.12
 25   3.9167      0.00    -0.02       0.00     0.64
 26   3.9168      0.00    -0.06       0.00     0.62
 27   3.9168      0.00     0.03       0.00     0.59
 28   3.9169      0.00    -0.07       0.00     0.64
 29   3.9169      0.00    -0.01       0.00     0.61
 30   3.9170      0.00     0.04       0.00     0.58
 31   3.9171      0.00     0.02       0.00     0.60
 32   4.0526      0.00     0.02       0.00    -0.69
 33   4.0526      0.00     0.02       0.00    -0.67
 34   4.0526      0.00    -0.07       0.00    -0.65
 35   4.0526      0.00    -0.08       0.00    -0.62
 36   4.0527      0.00     0.01       0.00    -0.70
 37   4.0528      0.00    -0.16       0.00    -0.67
 38   4.0528      0.00     0.06       0.00    -0.65
 39   4.0528      0.00     0.06       0.00    -0.73
 40   4.1305      0.00    -0.48       0.00    -0.52
 41   4.1306      0.00    -0.05       0.00     0.44
 42   4.1306      0.00    -0.22       0.00     0.48
 43   4.1308      0.00    -0.27       0.00     0.43
 44   4.1310      0.00    -0.60       0.00    -0.48
 45   4.1310      0.00    -0.51       0.00    -0.53
 46   4.1311      0.00    -0.13       0.00     0.40
 47   4.1312      0.00    -0.10       0.00     0.44
 48  16.0627      0.00    -0.07       0.00    -0.09
 49  16.0629      0.00     0.04       0.00    -0.12
 50  16.0630      0.00    -0.05       0.00    -0.16
 51  16.2925      0.00     0.23       0.00     0.19
 52  16.2926      0.00    -0.04       0.00     0.14

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.

03TJ58    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        44.793    44.793    44.793
ecceobj         0.094     0.094     0.094
incobj          0.954     0.954     0.954
qmin           39.443    39.441    39.439
qmax           49.778    49.790    49.765
amean          44.466    44.466    44.466
amin           44.109    44.107    44.109
amax           44.859    44.857    44.864
emean           0.094     0.094     0.094
emin            0.077     0.077     0.077
emax            0.111     0.111     0.110
imean           1.308     1.308     1.308
imin            0.440     0.440     0.440
imax            2.001     2.001     2.000
excite_mean     0.097     0.097     0.097
fracstop        1.000     1.000     1.000
cjmean          3.096     3.096     3.096

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       187.2     187.2     187.3
kozaiamp        180.0     180.0     180.0