Orbit Fit and Astrometric record for 04TE282

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: 04TE282   
# Created Fri Dec 14 02:08:39 2018
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting   24 observations of   24
# Arc:   9.95y
# First observation: 2004/10/15
#  Last observation: 2014/09/26
# Chi-squared of fit:    23.57 DOF:   42 RMS:  0.18
# Min/Max residuals:    -0.40    0.63
# Exact a, adot, b, bdot, g, gdot:
  1.595920E-05  3.382945E-02  5.311852E-06  1.267438E-02  3.188931E-02 -4.699044E-03
# Covariance matrix:
  2.2607E-13 -7.3338E-14  2.4290E-14 -1.7833E-14  5.2408E-14 -1.3071E-13
 -7.3338E-14  4.6361E-14 -2.0202E-14  1.5017E-14  1.8602E-14  1.0859E-13
  2.4290E-14 -2.0202E-14  1.4881E-13 -2.9472E-14 -1.4830E-14 -5.5094E-14
 -1.7833E-14  1.5017E-14 -2.9472E-14  1.1800E-14  1.1811E-14  4.1038E-14
  5.2408E-14  1.8602E-14 -1.4830E-14  1.1811E-14  2.7727E-13  7.9224E-14
 -1.3071E-13  1.0859E-13 -5.5094E-14  4.1038E-14  7.9224E-14  2.9609E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
    1.842230   51.424846    0.488435    0.028168   -0.872846  2453293.929253
# Heliocentric elements and errors
Epoch:              2453294.5000  =  2004/10/16
Mean Anomaly:          302.15902 +/-     0.013
Argument of Peri:       79.85918 +/-     0.017
Long of Asc Node:       45.81386 +/-     0.000
Inclination:            20.70308 +/-     0.000
Eccentricity:         0.15860657 +/-    0.0000
Semi-Major Axis:     34.44129250 +/-    0.0025
Time of Perihelion: 2465156.3036 +/-       7.1
Perihelion:          28.97867733 +/-    0.0023
Aphelion:            39.90390766 +/-    0.0030
Period (y)              202.1284 +/-      0.02
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           20.46495315 +/-    0.0003
Ecliptic Y           24.88244113 +/-    0.0004
Ecliptic Z            1.00826353 +/-    0.0000
Ecliptic XDOT        -0.00254531 +/-    0.0000
Ecliptic YDOT         0.00146130 +/-    0.0000
Ecliptic ZDOT         0.00107472 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   32.23308956 +/-    0.0004
Geocenter to KBO     31.35857830 +/-    0.0005
# Hcoef:  8.33

The following table shows the complete astrometric record for 04TE282. 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 (04TE282) followed by the observatory code and reference code for the source of the astrometry.

2004 10  15.42851  03 13 57.10   +19 53 45.3   22.8R 04TE282   695  Cl8661      
2004 10  15.50510  03 13 56.63   +19 53 44.0         04TE282   695  Cl8661      
2004 10  16.48805  03 13 51.00   +19 53 31.2         04TE282   695  Cl8661      
2004 11  09.25460  03 11 20.64   +19 47 07.1   22.8R 04TE282   695  Cl9882      
2004 11  09.34728  03 11 20.02   +19 47 06.0         04TE282   695  Cl9882      
2005 12  02.21336  03 16 02.25   +20 53 23.5   22.5R 04TE282   695  Cs2691      
2005 12  02.26607  03 16 01.90   +20 53 22.6         04TE282   695  Cs2691      
2005 12  02.31891  03 16 01.56   +20 53 21.7         04TE282   695  Cs2691      
2006 08  21.34359  03 31 04.19   +22 15 03.9   22.4R 04TE282   807  Cs2691      
2006 08  22.32785  03 31 04.86   +22 15 19.1         04TE282   807  Cs2691      
2006 08  23.31538  03 31 05.35   +22 15 34.9         04TE282   807  Cs2691      
2008 09  26.37949  03 45 26.53   +24 40 00.1   24.4R 04TE282   250  S~06Al      
2008 09  26.38574  03 45 26.51   +24 40 00.1         04TE282   250  S~06Al      
2008 09  26.39268  03 45 26.49   +24 40 00.2         04TE282   250  S~06Al      
2008 09  26.39893  03 45 26.47   +24 40 00.2         04TE282   250  S~06Al      
2008 10  23.45870  03 43 13.73   +24 39 22.1   24.4r 04TE282   695  C~0gMC      
2008 10  23.50962  03 43 13.44   +24 39 21.6   22.9r 04TE282   695  C~0gMC      
2008 10  24.37932  03 43 08.11   +24 39 15.4   22.7r 04TE282   695  C~0gMC      
2008 12  21.30401  03 36 41.28   +24 25 22.6   22.9r 04TE282   695  C~0hkR      
2008 12  21.37792  03 36 40.84   +24 25 21.3   23.2r 04TE282   695  C~0hkR      
2008 12  22.25068  03 36 35.92   +24 25 06.9   22.6r 04TE282   695  C~0hkR      
2014 09  26.36969  04 37 14.54   +31 12 28.4   23.9R 04TE282   695  C~1LJM      
2014 09  26.41488  04 37 14.47   +31 12 29.5         04TE282   695  C~1LJM      
2014 09  26.45944  04 37 14.38   +31 12 30.3         04TE282   695  C~1LJN      

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     0.12       0.00     0.24
  2   0.0002      0.00    -0.27       0.00    -0.06
  3   0.0029      0.00    -0.02       0.00    -0.09
  4   0.0680      0.00     0.17       0.00    -0.40
  5   0.0682      0.00     0.27       0.00     0.20
  6   1.1301      0.00     0.02       0.00    -0.17
  7   1.1303      0.00    -0.14       0.00    -0.11
  8   1.1304      0.00    -0.13       0.00    -0.03
  9   1.8478      0.00    -0.06       0.00     0.07
 10   1.8505      0.00     0.29       0.00    -0.14
 11   1.8532      0.00    -0.18       0.00     0.63
 12   3.9478      0.00     0.01       0.00    -0.00
 13   3.9479      0.00     0.03       0.00    -0.03
 14   3.9479      0.00     0.10       0.00     0.04
 15   3.9479      0.00     0.12       0.00     0.01
 16   4.0220      0.00    -0.36       0.00     0.15
 17   4.0221      0.00     0.02       0.00     0.02
 18   4.0245      0.00    -0.08       0.00     0.03
 19   4.1831      0.00     0.24       0.00    -0.04
 20   4.1833      0.00     0.03       0.00    -0.07
 21   4.1857      0.00     0.02       0.00    -0.03
 22   9.9465      0.00    -0.26       0.00    -0.07
 23   9.9466      0.00     0.10       0.00     0.08
 24   9.9467      0.00     0.16       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.

04TE282    quality flag:3

Type:       CENTAURR  CENTAURR  CENTAURR

axisobj        34.719    34.719    34.719
ecceobj         0.158     0.158     0.158
incobj         20.618    20.618    20.618
qmin           25.069    27.095    26.863
qmax           44.158    41.990    42.322
amean          33.952    34.424    34.419
amin           33.023    33.495    33.716
amax           36.952    34.949    34.873
emean           0.202     0.178     0.184
emin            0.128     0.117     0.139
emax            0.255     0.211     0.219
imean          19.630    19.273    21.043
imin           17.991    18.361    18.358
imax           22.353    20.551    25.004
excite_mean     0.393     0.376     0.404
fracstop        0.341     0.096     0.488
cjmean          2.845     2.853     2.833

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       181.5     191.6     176.0
kozaiamp        179.9     119.0     180.0