Orbit Fit and Astrometric record for 13TE172

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: 13TE172   
# Created Wed Dec 25 02:09:37 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     50 observations of     50
# Arc:   9.15y
# First observation: 2013/10/04
#  Last observation: 2022/11/28
# Chi-squared of fit:    29.48 DOF:     94 RMS:  0.14
# Min/Max residuals:    -0.30    0.36
# Exact a, adot, b, bdot, g, gdot:
  1.696279E-05  3.033752E-02  8.715179E-06  1.523995E-02  2.875653E-02  7.116220E-04
# Covariance matrix:
  2.5251E-13 -9.5832E-14  5.7807E-14 -3.7848E-14  4.1616E-14 -2.7319E-13
 -9.5832E-14  4.9246E-14 -3.6556E-14  2.2558E-14 -4.9776E-16  1.6055E-13
  5.7807E-14 -3.6556E-14  1.4072E-13 -4.4387E-14 -8.6434E-15 -1.4159E-13
 -3.7848E-14  2.2558E-14 -4.4387E-14  1.9896E-14  1.3531E-15  8.7128E-14
  4.1616E-14 -4.9776E-16 -8.6434E-15  1.3531E-15  7.4519E-14  2.6481E-15
 -2.7319E-13  1.6055E-13 -1.4159E-13  8.7128E-14  2.6481E-15  6.1968E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
  -14.515951   25.202080    0.247605   -0.242815   -0.938278  2456569.774008
# Heliocentric elements and errors
Epoch:              2456570.5000  =  2013/10/05
Mean Anomaly:            2.49540 +/-     0.003
Argument of Peri:      326.18251 +/-     0.006
Long of Asc Node:       50.84840 +/-     0.000
Inclination:            29.81323 +/-     0.000
Eccentricity:         0.26241873 +/-    0.0000
Semi-Major Axis:     48.39218360 +/-    0.0031
Time of Perihelion: 2455718.1885 +/-       1.2
Perihelion:          35.69316800 +/-    0.0030
Aphelion:            61.09119920 +/-    0.0043
Period (y)              336.6441 +/-      0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           31.44188769 +/-    0.0003
Ecliptic Y           14.52646860 +/-    0.0001
Ecliptic Z           -8.71600524 +/-    0.0001
Ecliptic XDOT        -0.00084766 +/-    0.0000
Ecliptic YDOT         0.00279486 +/-    0.0000
Ecliptic ZDOT         0.00138780 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   35.71524322 +/-    0.0003
Geocenter to KBO     34.77473090 +/-    0.0003
# Hcoef:  7.10

The following table shows the complete astrometric record for 13TE172. 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 (13TE172) followed by the observatory code and reference code for the source of the astrometry.

2013 10  04.27323  01 54 28.053  -03 47 02.35  23.5g 13TE172   W84  C~4yR9      
2013 10  27.12974  01 52 23.437  -03 55 53.27  23.5g 13TE172   W84  C~4yR9      
2013 11  13.12040  01 50 51.968  -03 59 42.66  22.3z 13TE172   W84  C~4yR9      
2014 08  18.37542  02 02 31.057  -01 59 53.00  22.0z 13TE172   W84  C~4yR9      
2014 10  02.34232  01 59 52.729  -02 19 39.17  23.3g 13TE172   W84  C~4yR9      
2014 12  25.09950  01 53 24.87   -02 30 02.6   21.9r 13TE172   W84  C~3clO      
2014 12  26.06520  01 53 22.918  -02 29 42.47  22.2z 13TE172   W84  C~4yR9      
2014 12  26.06658  01 53 22.906  -02 29 42.65  22.3i 13TE172   W84  C~4yR9      
2015 01  16.054294 01 53 04.54   -02 19 53.0   22.4z 13TE172   W84  C~35bZ      
2015 01  16.05482  01 53 04.558  -02 19 52.96  22.8z 13TE172   W84  C~4yR9      
2015 01  19.049792 01 53 05.80   -02 18 06.1   22.4z 13TE172   W84  C~35bZ      
2015 01  19.05031  01 53 05.815  -02 18 06.02  22.7z 13TE172   W84  C~4yR9      
2016 01  12.05868  01 58 09.441  -00 58 05.59  22.3r 13TE172   W84  C~4yR9      
2016 01  12.059514 01 58 09.46   -00 58 05.7   23.0g 13TE172   W84  C~35bZ      
2016 01  12.06004  01 58 09.462  -00 58 05.74  22.7g 13TE172   W84  C~4yR9      
2016 09  10.296157 02 11 47.38   +00 41 44.8   22.8r 13TE172   W84  C~35bZ      
2016 09  10.29669  02 11 47.381  +00 41 44.80  23.0r 13TE172   W84  C~4yR9      
2016 09  10.29806  02 11 47.372  +00 41 44.95  24.0g 13TE172   W84  C~4yR9      
2016 09  10.39463  02 11 47.033  +00 41 42.62  22.4z 13TE172   W84  C~4yR9      
2016 10  27.16787  02 07 59.608  +00 22 56.84  22.3r 13TE172   W84  C~4yR9      
2016 10  27.16927  02 07 59.605  +00 22 56.81  22.2i 13TE172   W84  C~4yR9      
2016 10  27.170104 02 07 59.57   +00 22 56.6   23.4g 13TE172   W84  C~35bZ      
2016 11  07.17116  02 06 58.635  +00 19 49.11  22.4z 13TE172   W84  C~4yR9      
2016 11  11.18165  02 06 36.969  +00 18 54.87  22.5z 13TE172   W84  C~4yR9      
2016 11  27.126840 02 05 16.96   +00 16 48.9   22.7r 13TE172   W84  C~35bZ      
2016 11  27.12737  02 05 16.964  +00 16 48.85  22.8r 13TE172   W84  C~4yR9      
2016 11  28.11615  02 05 12.42   +00 16 46.1   22.2i 13TE172   W84  C~3clO      
2016 11  28.117002 02 05 12.41   +00 16 46.3   23.2g 13TE172   W84  C~35bZ      
2016 12  23.23522  02 03 42.30   +00 19 17.4   22.8z 13TE172   T09  C~7bID      
2016 12  23.33073  02 03 42.06   +00 19 18.9   22.3z 13TE172   T09  C~7bID      
2016 12  23.34086  02 03 42.03   +00 19 18.9   22.4z 13TE172   T09  C~7bID      
2016 12  23.38550  02 03 41.90   +00 19 19.8   22.6z 13TE172   T09  C~7bID      
2016 12  23.39357  02 03 41.88   +00 19 19.9   22.8z 13TE172   T09  C~7bID      
2016 12  23.39624  02 03 41.88   +00 19 20.0   22.3z 13TE172   T09  C~7bID      
2017 08  27.408981 02 17 34.56   +02 11 56.5   22.4i 13TE172   W84  C~35bZ      
2017 08  27.40951  02 17 34.563  +02 11 56.47  22.2i 13TE172   W84  C~4yR9      
2017 08  27.41993  02 17 34.534  +02 11 56.05  22.6z 13TE172   W84  C~4yR9      
2017 09  18.334687 02 16 26.60   +02 04 00.7   22.6r 13TE172   W84  C~35bZ      
2017 09  18.33522  02 16 26.598  +02 04 00.64  22.6r 13TE172   W84  C~4yR9      
2017 09  18.336088 02 16 26.58   +02 04 00.6   23.3g 13TE172   W84  C~35bZ      
2017 09  18.33661  02 16 26.587  +02 04 00.44  22.8g 13TE172   W84  C~4yR9      
2017 10  27.253773 02 13 10.96   +01 48 57.3   23.7g 13TE172   W84  C~35bZ      
2017 10  27.25430  02 13 10.962  +01 48 57.21  23.4g 13TE172   W84  C~4yR9      
2017 11  01.164572 02 12 43.54   +01 47 25.2   22.1z 13TE172   W84  C~35ba      
2017 11  01.16510  02 12 43.538  +01 47 25.28  22.3z 13TE172   W84  C~4yR9      
2018 09  09.28945  02 22 07.925  +03 32 27.70  22.5z 13TE172   W84  C~4yR9      
2018 10  20.21247  02 19 01.610  +03 17 06.92  22.5z 13TE172   W84  C~4yR9      
2022 11  28.244860 02 36 11.262  +08 44 58.81  22.7G 13TE172   G37  C~675S      
2022 11  28.295660 02 36 10.992  +08 44 58.60        13TE172   G37  C~675S      
2022 11  28.345250 02 36 10.738  +08 44 57.83        13TE172   G37  C~675S      

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    -0.03       0.00    -0.09
     2   0.0626      0.00     0.15       0.00     0.00
     3   0.1091      0.00    -0.01       0.00    -0.01
     4   0.8709      0.00    -0.18       0.00     0.22
     5   0.9940      0.00     0.03       0.00     0.04
     6   1.2233      0.00     0.12       0.00    -0.21
     7   1.2260      0.00     0.22       0.00     0.08
     8   1.2260      0.00     0.09       0.00    -0.13
     9   1.2835      0.00    -0.12       0.00     0.03
    10   1.2835      0.00     0.15       0.00     0.06
    11   1.2917      0.00    -0.30       0.00    -0.23
    12   1.2917      0.00    -0.07       0.00    -0.17
    13   2.2718      0.00     0.04       0.00     0.04
    14   2.2718      0.00     0.33       0.00    -0.09
    15   2.2718      0.00     0.36       0.00    -0.15
    16   2.9350      0.00    -0.02       0.00    -0.10
    17   2.9350      0.00     0.02       0.00    -0.09
    18   2.9350      0.00    -0.04       0.00     0.09
    19   2.9353      0.00     0.07       0.00     0.11
    20   3.0634      0.00     0.08       0.00     0.06
    21   3.0634      0.00     0.16       0.00     0.06
    22   3.0634      0.00    -0.30       0.00    -0.13
    23   3.0935      0.00     0.04       0.00     0.04
    24   3.1045      0.00     0.10       0.00    -0.07
    25   3.1481      0.00    -0.03       0.00     0.15
    26   3.1481      0.00     0.07       0.00     0.10
    27   3.1508      0.00    -0.20       0.00     0.07
    28   3.1508      0.00    -0.29       0.00     0.28
    29   3.2196      0.00    -0.02       0.00     0.01
    30   3.2199      0.00     0.08       0.00     0.11
    31   3.2199      0.00     0.02       0.00    -0.04
    32   3.2200      0.00    -0.22       0.00     0.20
    33   3.2200      0.00    -0.21       0.00     0.18
    34   3.2200      0.00    -0.11       0.00     0.24
    35   3.8963      0.00     0.05       0.00     0.05
    36   3.8963      0.00     0.12       0.00     0.03
    37   3.8964      0.00     0.03       0.00    -0.20
    38   3.9564      0.00     0.07       0.00     0.14
    39   3.9564      0.00     0.07       0.00     0.09
    40   3.9564      0.00    -0.15       0.00     0.07
    41   3.9564      0.00    -0.01       0.00    -0.08
    42   4.0629      0.00    -0.08       0.00     0.04
    43   4.0629      0.00    -0.01       0.00    -0.03
    44   4.0764      0.00    -0.00       0.00    -0.30
    45   4.0764      0.00     0.01       0.00    -0.21
    46   4.9309      0.00     0.14       0.00     0.04
    47   5.0430      0.00    -0.01       0.00    -0.09
    48   9.1498      0.00     0.11       0.00    -0.14
    49   9.1500      0.00    -0.02       0.00     0.16
    50   9.1501      0.00    -0.00       0.00    -0.12

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.

13TE172    quality flag:3

Type:       SCATNEAR  SCATNEAR  SCATNEAR

axisobj        48.730    48.730    48.730
ecceobj         0.268     0.268     0.268
incobj         29.794    29.794    29.794
qmin           34.239    34.257    34.248
qmax           62.859    62.882    62.862
amean          48.264    48.269    48.257
amin           47.785    47.772    47.783
amax           48.823    48.829    48.814
emean           0.266     0.266     0.266
emin            0.243     0.243     0.243
emax            0.289     0.289     0.289
imean          28.705    28.712    28.703
imin           28.049    28.041    28.049
imax           29.271    29.281    29.271
excite_mean     0.549     0.549     0.549
fracstop        1.000     1.000     1.000
cjmean          2.765     2.765     2.765

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       168.7     169.0     168.6
kozaiamp        180.0     180.0     179.9