Orbit Fit and Astrometric record for 10TD192

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: 10TD192   
# Created Sat Mar 30 01:13:56 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     21 observations of     21
# Arc:   9.28y
# First observation: 2010/10/08
#  Last observation: 2020/01/18
# Chi-squared of fit:    21.81 DOF:     36 RMS:  0.18
# Min/Max residuals:    -0.55    0.51
# Exact a, adot, b, bdot, g, gdot:
  1.498096E-05  2.372273E-02  9.139543E-07  1.546751E-03  2.424350E-02  4.802853E-04
# Covariance matrix:
  2.2890E-13 -8.8676E-14  4.0112E-15 -5.4854E-15  1.6607E-13 -4.3293E-13
 -8.8676E-14  1.3602E-13 -5.6338E-15  9.0728E-15  4.0860E-14  7.2827E-13
  4.0112E-15 -5.6338E-15  1.2876E-13 -2.1447E-14  1.2078E-15 -3.2809E-14
 -5.4854E-15  9.0728E-15 -2.1447E-14  8.5954E-15  8.8165E-16  5.2108E-14
  1.6607E-13  4.0860E-14  1.2078E-15  8.8165E-16  5.5741E-13  9.2176E-14
 -4.3293E-13  7.2827E-13 -3.2809E-14  5.2108E-14  9.2176E-14  4.1772E-12
#      lat0       lon0       xBary       yBary       zBary        JD0
   -2.272931   46.613799    0.521912   -0.033641   -0.847065  2455477.907366
# Heliocentric elements and errors
Epoch:              2455478.5000  =  2010/10/09
Mean Anomaly:           17.49843 +/-     0.139
Argument of Peri:      310.32411 +/-     0.149
Long of Asc Node:       76.90684 +/-     0.001
Inclination:             4.31657 +/-     0.000
Eccentricity:         0.03074103 +/-    0.0001
Semi-Major Axis:     43.36813042 +/-    0.0055
Time of Perihelion: 2450407.9979 +/-      40.4
Perihelion:          42.03494942 +/-    0.0070
Aphelion:            44.70131143 +/-    0.0072
Period (y)              285.6040 +/-      0.05
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           29.27695569 +/-    0.0009
Ecliptic Y           30.20986739 +/-    0.0009
Ecliptic Z           -1.63584859 +/-    0.0001
Ecliptic XDOT        -0.00190483 +/-    0.0000
Ecliptic YDOT         0.00189105 +/-    0.0000
Ecliptic ZDOT         0.00017238 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   42.10049538 +/-    0.0009
Geocenter to KBO     41.24817551 +/-    0.0013
# Hcoef:  6.58

The following table shows the complete astrometric record for 10TD192. 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 (10TD192) followed by the observatory code and reference code for the source of the astrometry.

2010 10  08.40660  02 59 16.288  +14 37 24.57  23.3w 10TD192   F51  C~1w3k      
2010 10  08.44303  02 59 16.114  +14 37 23.68  23.1w 10TD192   F51  C~1w3k      
2010 10  09.45394  02 59 12.064  +14 37 05.74  23.3w 10TD192   F51  C~1w3k      
2010 10  09.47005  02 59 12.009  +14 37 05.24  23.2w 10TD192   F51  C~1w3k      
2010 11  08.48022  02 56 54.320  +14 27 14.31  22.9w 10TD192   F51  C~1w3k      
2010 11  08.49297  02 56 54.271  +14 27 14.09  23.1w 10TD192   F51  C~1w3k      
2010 11  08.50717  02 56 54.194  +14 27 13.43  23.4w 10TD192   F51  C~1w3k      
2010 11  08.51986  02 56 54.131  +14 27 13.35  23.2w 10TD192   F51  C~1w3k      
2011 12  02.26789  03 00 21.257  +14 48 12.42  21.8i 10TD192   F51  C~1w3k      
2011 12  02.29340  03 00 21.130  +14 48 12.11  22.0r 10TD192   F51  C~1w3k      
2012 10  18.39688  03 09 10.899  +15 29 45.99  22.8w 10TD192   F51  C~1w3k      
2012 10  18.42719  03 09 10.777  +15 29 45.83  22.9w 10TD192   F51  C~1w3k      
2012 10  18.44246  03 09 10.704  +15 29 45.41  22.8w 10TD192   F51  C~1w3k      
2013 11  24.31473  03 11 36.418  +15 45 36.77  22.7w 10TD192   F51  C~1w3k      
2013 11  24.34140  03 11 36.281  +15 45 36.21  22.8w 10TD192   F51  C~1w3k      
2017 10  28.32104  03 35 23.10   +17 37 04.3         10TD192   G37  C~3cg0      
2017 10  28.41059  03 35 22.68   +17 37 02.9         10TD192   G37  C~3cg0      
2017 10  28.45293  03 35 22.49   +17 37 02.4         10TD192   G37  C~3cg0      
2017 10  28.49558  03 35 22.29   +17 37 01.6         10TD192   G37  C~3cg0      
2020 01  18.160450 03 40 28.557  +18 08 24.70  23.5G 10TD192   G37  C~3j0l      
2020 01  18.277360 03 40 28.233  +18 08 23.86        10TD192   G37  C~3j0l      

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     0.05
     2   0.0001      0.00    -0.30       0.00    -0.19
     3   0.0029      0.00    -0.14       0.00     0.10
     4   0.0029      0.00     0.03       0.00    -0.11
     5   0.0851      0.00    -0.03       0.00     0.15
     6   0.0851      0.00     0.19       0.00     0.19
     7   0.0851      0.00     0.09       0.00    -0.18
     8   0.0852      0.00     0.09       0.00    -0.00
     9   1.1495      0.00     0.01       0.00     0.07
    10   1.1496      0.00    -0.15       0.00     0.18
    11   2.0287      0.00    -0.09       0.00    -0.37
    12   2.0288      0.00     0.11       0.00     0.01
    13   2.0288      0.00     0.05       0.00    -0.13
    14   3.1291      0.00     0.01       0.00     0.07
    15   3.1292      0.00    -0.09       0.00    -0.02
    16   7.0552      0.00    -0.05       0.00     0.03
    17   7.0555      0.00    -0.03       0.00     0.05
    18   7.0556      0.00     0.11       0.00     0.23
    19   7.0557      0.00     0.11       0.00     0.12
    20   9.2779      0.00     0.51       0.00     0.04
    21   9.2782      0.00    -0.55       0.00    -0.30

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.

10TD192    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        43.543    43.543    43.543
ecceobj         0.034     0.034     0.034
incobj          4.312     4.312     4.312
qmin           40.698    40.700    40.697
qmax           45.880    45.881    45.879
amean          43.209    43.209    43.209
amin           42.873    42.873    42.873
amax           43.558    43.558    43.558
emean           0.037     0.037     0.037
emin            0.017     0.017     0.017
emax            0.054     0.054     0.054
imean           2.526     2.526     2.526
imin            1.619     1.619     1.619
imax            3.427     3.427     3.427
excite_mean     0.058     0.058     0.058
fracstop        1.000     1.000     1.000
cjmean          3.088     3.088     3.088

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       173.2     173.2     173.2
kozaiamp        179.9     180.0     179.9