Orbit Fit and Astrometric record for 13PD84

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: 13PD84    
# Created Sun Nov 24 02:09:26 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     65 observations of     65
# Arc:  12.12y
# First observation: 2012/08/17
#  Last observation: 2024/10/01
# Chi-squared of fit:    73.86 DOF:    124 RMS:  0.19
# Min/Max residuals:    -0.62    0.79
# Exact a, adot, b, bdot, g, gdot:
  1.865073E-05  2.996231E-02  6.168896E-06  9.492756E-03  2.569467E-02  7.789284E-03
# Covariance matrix:
  1.5889E-13 -7.4007E-14  3.3995E-14 -2.0467E-14 -7.9071E-15 -1.8942E-13
 -7.4007E-14  4.2174E-14 -2.0816E-14  1.2557E-14  2.9435E-15  1.1621E-13
  3.3995E-14 -2.0816E-14  6.9861E-14 -1.9539E-14 -5.1772E-16 -6.4577E-14
 -2.0467E-14  1.2557E-14 -1.9539E-14  8.8259E-15 -8.3800E-16  3.9173E-14
 -7.9071E-15  2.9435E-15 -5.1772E-16 -8.3800E-16  8.8801E-14 -7.6245E-15
 -1.8942E-13  1.1621E-13 -6.4577E-14  3.9173E-14 -7.6245E-15  3.6251E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
   -8.995418  -29.362473    0.106706   -0.157356   -0.993921  2456156.947108
# Heliocentric elements and errors
Epoch:              2456156.5000  =  2012/08/17
Mean Anomaly:            6.56416 +/-     0.002
Argument of Peri:      297.01171 +/-     0.002
Long of Asc Node:      356.31935 +/-     0.000
Inclination:            19.49470 +/-     0.000
Eccentricity:         0.63283532 +/-    0.0001
Semi-Major Axis:    100.74505446 +/-    0.0175
Time of Perihelion: 2449421.9216 +/-       2.5
Perihelion:          36.99002611 +/-    0.0089
Aphelion:           164.50008281 +/-    0.0293
Period (y)             1011.2157 +/-      0.26
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           34.32892950 +/-    0.0004
Ecliptic Y          -19.43199070 +/-    0.0002
Ecliptic Z           -6.08485557 +/-    0.0001
Ecliptic XDOT         0.00241208 +/-    0.0000
Ecliptic YDOT         0.00230573 +/-    0.0000
Ecliptic ZDOT         0.00086939 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   39.91351246 +/-    0.0004
Geocenter to KBO     38.91842687 +/-    0.0005
# Hcoef:  6.77

The following table shows the complete astrometric record for 13PD84. 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 (13PD84) followed by the observatory code and reference code for the source of the astrometry.

2012 08  17.44633  22 24 14.884  -19 38 21.50  22.7G 13PD84    F51  C~346H      
2012 08  17.46062  22 24 14.813  -19 38 21.58  22.2G 13PD84    F51  C~346H      
2012 08  17.47488  22 24 14.743  -19 38 22.18  22.8G 13PD84    F51  C~346H      
2012 08  17.48915  22 24 14.681  -19 38 21.96  21.8G 13PD84    F51  C~346H      
2013 08  09.44376  22 30 44.034  -18 27 03.79  22.5G 13PD84    F51  C~346H      
2013 08  09.45801  22 30 43.983  -18 27 04.08  22.3G 13PD84    F51  C~346H      
2013 08  09.47225  22 30 43.914  -18 27 04.68  21.9G 13PD84    F51  C~346H      
2013 08  09.48649  22 30 43.832  -18 27 05.01  22.9G 13PD84    F51  C~346H      
2013 10  06.31318  22 26 18.908  -18 43 31.88  22.7G 13PD84    F51  C~346H      
2013 10  06.32743  22 26 18.854  -18 43 32.21  22.5G 13PD84    F51  C~346H      
2013 10  06.34167  22 26 18.808  -18 43 32.09  22.6G 13PD84    F51  C~346H      
2013 10  06.35593  22 26 18.757  -18 43 32.01  22.5G 13PD84    F51  C~346H      
2014 06  28.56088  22 38 42.534  -17 04 33.67  22.7G 13PD84    F51  C~346H      
2014 06  28.57277  22 38 42.486  -17 04 33.38  22.9G 13PD84    F51  C~346H      
2014 06  28.58463  22 38 42.477  -17 04 34.00  23.1G 13PD84    F51  C~346H      
2014 06  28.59652  22 38 42.478  -17 04 33.95  23.1G 13PD84    F51  C~346H      
2014 07  06.55632  22 38 25.497  -17 06 51.05  22.9G 13PD84    F51  C~346H      
2014 07  08.53602  22 38 20.492  -17 07 28.58  22.5G 13PD84    F51  C~346H      
2014 07  08.54782  22 38 20.455  -17 07 28.83  23.0G 13PD84    F51  C~346H      
2014 07  08.55963  22 38 20.434  -17 07 28.96  22.7G 13PD84    F51  C~346H      
2014 07  08.57143  22 38 20.416  -17 07 29.51  23.0G 13PD84    F51  C~346H      
2014 07  29.50488  22 37 10.540  -17 15 03.25  22.4G 13PD84    F51  C~346H      
2014 07  29.51634  22 37 10.488  -17 15 03.63  22.6G 13PD84    F51  C~346H      
2014 07  29.52779  22 37 10.451  -17 15 03.70  23.0G 13PD84    F51  C~346H      
2014 07  29.53926  22 37 10.356  -17 15 04.11  21.7G 13PD84    F51  C~346H      
2014 09  18.38388  22 33 15.288  -17 33 21.02  22.5G 13PD84    F51  C~346H      
2014 09  18.39508  22 33 15.220  -17 33 21.22  23.2G 13PD84    F51  C~346H      
2014 09  18.40627  22 33 15.158  -17 33 21.63  23.3G 13PD84    F51  C~346H      
2014 09  18.41745  22 33 15.152  -17 33 21.65  22.3G 13PD84    F51  C~346H      
2014 09  20.33076  22 33 06.544  -17 33 49.99  22.7G 13PD84    F51  C~346H      
2014 09  20.34196  22 33 06.465  -17 33 50.20  22.7G 13PD84    F51  C~346H      
2014 09  20.35586  22 33 06.367  -17 33 50.59  22.6G 13PD84    F51  C~346H      
2014 09  20.36705  22 33 06.351  -17 33 50.45  23.1G 13PD84    F51  C~346H      
2014 09  21.06449  22 33 03.26   -17 34 00.4   23.2V 13PD84    W84  C~346H      
2014 09  21.15296  22 33 02.86   -17 34 01.6         13PD84    W84  C~346H      
2014 09  21.21439  22 33 02.58   -17 34 02.4         13PD84    W84  C~346H      
2015 06  17.60270  22 44 19.225  -15 55 51.37  23.0G 13PD84    F51  C~346H      
2015 06  20.58400  22 44 16.815  -15 56 22.25  22.4G 13PD84    F51  C~346H      
2015 07  24.48424  22 42 57.970  -16 06 08.07  22.7G 13PD84    F51  C~346H      
2015 08  10.47209  22 41 50.017  -16 12 42.12  22.4G 13PD84    F51  C~346H      
2015 08  10.48396  22 41 49.964  -16 12 42.53  22.7G 13PD84    F51  C~346H      
2015 08  10.49587  22 41 49.916  -16 12 42.83  22.8G 13PD84    F51  C~346H      
2015 08  10.50777  22 41 49.848  -16 12 43.28  22.7G 13PD84    F51  C~346H      
2015 08  11.47589  22 41 45.581  -16 13 06.31  22.5G 13PD84    F51  C~346H      
2015 08  11.48781  22 41 45.553  -16 13 06.38  22.2G 13PD84    F51  C~346H      
2015 08  11.51159  22 41 45.452  -16 13 07.12  21.7G 13PD84    F51  C~346H      
2015 08  12.46879  22 41 41.172  -16 13 29.74  22.3G 13PD84    F51  C~346H      
2015 08  12.48071  22 41 41.135  -16 13 30.06  22.8G 13PD84    F51  C~346H      
2015 08  12.49261  22 41 41.079  -16 13 30.30  22.1G 13PD84    F51  C~346H      
2015 08  12.50453  22 41 41.007  -16 13 30.52  22.2G 13PD84    F51  C~346H      
2016 07  07.53750  22 49 02.631  -14 54 41.84  22.9G 13PD84    F51  C~346H      
2016 07  07.54874  22 49 02.588  -14 54 41.91  22.9G 13PD84    F51  C~346I      
2016 07  07.55996  22 49 02.587  -14 54 42.20  22.9G 13PD84    F51  C~346I      
2016 07  07.57116  22 49 02.559  -14 54 42.30  22.7G 13PD84    F51  C~346I      
2016 08  03.50839  22 47 35.844  -15 03 54.46  23.2G 13PD84    F51  C~346I      
2016 08  03.51942  22 47 35.797  -15 03 54.64  23.1G 13PD84    F51  C~346I      
2016 08  03.53047  22 47 35.771  -15 03 54.70  22.5G 13PD84    F51  C~346I      
2016 08  03.54154  22 47 35.764  -15 03 54.53  23.1G 13PD84    F51  C~346I      
2016 10  25.25611  22 41 53.929  -15 26 10.59  22.8G 13PD84    F51  C~346I      
2016 10  25.26726  22 41 53.904  -15 26 10.52  23.0G 13PD84    F51  C~346I      
2016 10  25.27841  22 41 53.858  -15 26 10.37  22.7G 13PD84    F51  C~346I      
2016 10  25.28960  22 41 53.838  -15 26 10.40  23.5G 13PD84    F51  C~346I      
2024 10  01.230580 23 21 38.192  -07 03 10.12  22.9G 13PD84    G37  C~8GxL      
2024 10  01.269480 23 21 38.034  -07 03 11.00        13PD84    G37  C~8GxL      
2024 10  01.309170 23 21 37.874  -07 03 11.62        13PD84    G37  C~8GxL      

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    -0.02       0.00    -0.08
     2   0.0000      0.00    -0.01       0.00     0.17
     3   0.0001      0.00     0.01       0.00    -0.10
     4   0.0001      0.00     0.14       0.00     0.45
     5   0.9774      0.00    -0.08       0.00     0.15
     6   0.9774      0.00     0.16       0.00     0.20
     7   0.9775      0.00     0.12       0.00    -0.06
     8   0.9775      0.00    -0.11       0.00    -0.04
     9   1.1358      0.00     0.07       0.00    -0.00
    10   1.1359      0.00     0.05       0.00    -0.26
    11   1.1359      0.00     0.16       0.00    -0.06
    12   1.1360      0.00     0.18       0.00     0.09
    13   1.8621      0.00     0.08       0.00    -0.17
    14   1.8621      0.00    -0.30       0.00     0.31
    15   1.8621      0.00    -0.10       0.00    -0.12
    16   1.8621      0.00     0.25       0.00     0.11
    17   1.8839      0.00    -0.07       0.00     0.10
    18   1.8894      0.00    -0.02       0.00    -0.05
    19   1.8894      0.00    -0.10       0.00    -0.07
    20   1.8894      0.00     0.07       0.00     0.03
    21   1.8895      0.00     0.27       0.00    -0.30
    22   1.9468      0.00     0.07       0.00     0.14
    23   1.9468      0.00    -0.01       0.00     0.03
    24   1.9468      0.00     0.13       0.00     0.23
    25   1.9469      0.00    -0.59       0.00     0.09
    26   2.0861      0.00     0.08       0.00    -0.10
    27   2.0861      0.00    -0.17       0.00    -0.13
    28   2.0861      0.00    -0.32       0.00    -0.37
    29   2.0862      0.00     0.37       0.00    -0.21
    30   2.0914      0.00     0.32       0.00    -0.01
    31   2.0914      0.00    -0.10       0.00    -0.05
    32   2.0915      0.00    -0.62       0.00    -0.24
    33   2.0915      0.00    -0.10       0.00     0.06
    34   2.0934      0.00     0.05       0.00    -0.06
    35   2.0937      0.00     0.05       0.00     0.00
    36   2.0938      0.00     0.02       0.00     0.06
    37   2.8314      0.00     0.09       0.00     0.11
    38   2.8395      0.00    -0.19       0.00    -0.25
    39   2.9323      0.00     0.01       0.00     0.07
    40   2.9789      0.00     0.06       0.00     0.07
    41   2.9789      0.00     0.06       0.00    -0.06
    42   2.9789      0.00     0.14       0.00    -0.08
    43   2.9789      0.00    -0.08       0.00    -0.24
    44   2.9816      0.00    -0.21       0.00    -0.23
    45   2.9816      0.00     0.18       0.00    -0.01
    46   2.9817      0.00     0.27       0.00    -0.19
    47   2.9843      0.00    -0.28       0.00    -0.02
    48   2.9844      0.00    -0.02       0.00    -0.06
    49   2.9844      0.00    -0.05       0.00    -0.02
    50   2.9844      0.00    -0.32       0.00     0.05
    51   3.8880      0.00    -0.06       0.00     0.10
    52   3.8880      0.00    -0.30       0.00     0.22
    53   3.8881      0.00     0.08       0.00     0.12
    54   3.8881      0.00     0.06       0.00     0.21
    55   3.9618      0.00    -0.05       0.00    -0.14
    56   3.9619      0.00    -0.08       0.00    -0.07
    57   3.9619      0.00     0.21       0.00     0.13
    58   3.9619      0.00     0.79       0.00     0.55
    59   4.1884      0.00     0.11       0.00    -0.05
    60   4.1884      0.00     0.16       0.00     0.01
    61   4.1885      0.00    -0.11       0.00     0.16
    62   4.1885      0.00     0.01       0.00     0.12
    63  12.1226      0.00    -0.05       0.00     0.02
    64  12.1227      0.00    -0.02       0.00    -0.12
    65  12.1228      0.00     0.02       0.00     0.02

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.

13PD84    quality flag:3

Type:       SCATNEAR  SCATNEAR  SCATNEAR

axisobj       100.980   101.066   100.895
ecceobj         0.634     0.634     0.634
incobj         19.480    19.480    19.480
qmin           35.763    36.101    35.790
qmax          171.076   172.074   170.843
amean         100.905   101.391   100.969
amin           98.980    99.037    98.982
amax          103.889   104.668   104.172
emean           0.631     0.631     0.631
emin            0.617     0.617     0.616
emax            0.647     0.644     0.645
imean          20.502    20.824    20.539
imin           19.651    20.005    19.670
imax           21.490    21.530    21.606
excite_mean     0.722     0.724     0.722
fracstop        1.000     1.000     1.000
cjmean          2.958     2.959     2.959

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       151.5     140.8     150.7
kozaiamp        180.0     180.0     180.0