Orbit Fit and Astrometric record for 01PK47

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: 01PK47    
# Created Wed Dec 25 02:08:12 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     34 observations of     34
# Arc:  19.33y
# First observation: 2001/08/12
#  Last observation: 2020/12/09
# Chi-squared of fit:   199.78 DOF:     62 RMS:  0.43
# Min/Max residuals:    -1.03    0.96
# Exact a, adot, b, bdot, g, gdot:
  1.770453E-05  2.774442E-02 -3.448294E-06 -2.031544E-03  2.674865E-02 -8.380989E-04
# Covariance matrix:
  1.3790E-13 -2.0145E-14 -2.4393E-15  1.0980E-15  2.3171E-14 -2.6405E-14
 -2.0145E-14  1.1042E-14  1.5508E-15 -6.8768E-16  1.7481E-14  1.7585E-14
 -2.4393E-15  1.5508E-15  9.2462E-14 -7.5489E-15  2.0027E-15  2.7965E-15
  1.0980E-15 -6.8768E-16 -7.5489E-15  1.1146E-15 -8.6284E-16 -1.2423E-15
  2.3171E-14  1.7481E-14  2.0027E-15 -8.6284E-16  1.0060E-13  2.4641E-14
 -2.6405E-14  1.7585E-14  2.7965E-15 -1.2423E-15  2.4641E-14  3.1541E-14
#      lat0       lon0       xBary       yBary       zBary        JD0
    7.888417    6.820982    0.745410    0.094362   -0.681982  2452134.059513
# Heliocentric elements and errors
Epoch:              2452134.5000  =  2001/08/13
Mean Anomaly:          314.50155 +/-     0.017
Argument of Peri:      168.78202 +/-     0.020
Long of Asc Node:      248.18893 +/-     0.000
Inclination:             8.71668 +/-     0.000
Eccentricity:         0.06959047 +/-    0.0000
Semi-Major Axis:     39.91896169 +/-    0.0019
Time of Perihelion: 2463777.4064 +/-       7.2
Perihelion:          37.14098235 +/-    0.0020
Aphelion:            42.69694102 +/-    0.0022
Period (y)              252.2186 +/-      0.02
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           37.54403375 +/-    0.0004
Ecliptic Y            3.74592529 +/-    0.0001
Ecliptic Z            5.13077652 +/-    0.0001
Ecliptic XDOT        -0.00040192 +/-    0.0000
Ecliptic YDOT         0.00281440 +/-    0.0000
Ecliptic ZDOT        -0.00021754 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   38.07773275 +/-    0.0004
Geocenter to KBO     37.38512046 +/-    0.0004
# Hcoef:  7.22

The following table shows the complete astrometric record for 01PK47. 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 (01PK47) followed by the observatory code and reference code for the source of the astrometry.

2001 08  12.55877  00 12 25.08   +09 56 44.6   22.8  01PK47    568  Cd3473      
2001 08  12.59535  00 12 24.99   +09 56 44.2         01PK47    568  Cd3473      
2001 08  13.56727  00 12 21.82   +09 56 31.9         01PK47    568  Cd3473      
2001 08  13.61786  00 12 21.68   +09 56 31.3         01PK47    568  Cd3473      
2001 08  14.45066  00 12 18.89   +09 56 20.1         01PK47    568  Cd3473      
2001 08  14.48814  00 12 18.75   +09 56 19.4         01PK47    568  Cd3473      
2001 09  16.27513  00 09 59.30   +09 44 12.8         01PK47    695  Cd5903      
2001 09  16.32232  00 09 59.06   +09 44 11.3         01PK47    695  Cd5903      
2001 09  18.23620  00 09 49.77   +09 43 15.2         01PK47    695  Cd5903      
2001 09  18.27439  00 09 49.60   +09 43 13.8         01PK47    695  Cd5903      
2003 11  21.12677  00 17 41.63   +10 12 22.6   22.3R 01PK47    695  Co3500      
2003 11  21.17620  00 17 41.50   +10 12 21.1         01PK47    695  Co3500      
2005 09  30.29997  00 33 39.73   +11 43 15.7   22.2R 01PK47    688  Co3500      
2005 09  30.39800  00 33 39.23   +11 43 13.7         01PK47    688  Co3500      
2008 07  16.44685  00 56 26.79   +13 28 23.7   24.0R 01PK47    250  S~06AP      
2008 07  16.45310  00 56 26.79   +13 28 23.8         01PK47    250  S~06AP      
2008 07  16.51282  00 56 26.80   +13 28 24.4         01PK47    250  S~06AP      
2008 07  16.51907  00 56 26.80   +13 28 24.5         01PK47    250  S~06AP      
2008 11  02.346226 00 49 58.99   +12 54 57.8   22.4V 01PK47    645  C~1Q3A      
2008 11  02.347055 00 49 58.98   +12 54 57.8   23.1V 01PK47    645  C~1Q3A      
2008 11  02.349543 00 49 58.97   +12 54 57.7   23.6V 01PK47    645  C~1Q3A      
2009 12  10.54934  00 54 21.13   +13 05 33.3         01PK47    250  S~0M3L      
2009 12  10.55173  00 54 21.13   +13 05 33.2         01PK47    250  S~0M3L      
2009 12  10.58788  00 54 21.07   +13 05 32.4         01PK47    250  S~0M3L      
2009 12  10.59027  00 54 21.06   +13 05 32.4         01PK47    250  S~0M3L      
2009 12  10.59535  00 54 21.06   +13 05 32.6         01PK47    250  S~0M3L      
2009 12  10.60090  00 54 21.04   +13 05 32.5         01PK47    250  S~0M3L      
2009 12  10.60706  00 54 21.04   +13 05 32.4         01PK47    250  S~0M3L      
2009 12  10.61262  00 54 21.03   +13 05 32.3         01PK47    250  S~0M3L      
2018 09  14.321050 01 59 51.87   +17 41 38.3   23.3G 01PK47    705  C~2r9h      
2018 09  14.379860 01 59 51.64   +17 41 37.6   23.0G 01PK47    705  C~2r9h      
2018 09  14.436810 01 59 51.43   +17 41 36.6   22.7G 01PK47    705  C~2r9h      
2020 12  09.099350 02 06 38.648  +17 46 52.61  22.9G 01PK47    G37  C~4Tvw      
2020 12  09.154470 02 06 38.469  +17 46 51.13        01PK47    G37  C~4Tvw      

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    -0.44       0.00     0.32
     2   0.0001      0.00     0.05       0.00     0.36
     3   0.0028      0.00     0.47       0.00     0.17
     4   0.0029      0.00     0.96       0.00     0.22
     5   0.0052      0.00     0.85       0.00    -0.11
     6   0.0053      0.00     0.70       0.00    -0.32
     7   0.0950      0.00    -0.21       0.00    -0.93
     8   0.0952      0.00    -0.33       0.00    -1.03
     9   0.1004      0.00    -0.50       0.00     0.19
    10   0.1005      0.00    -0.22       0.00    -0.05
    11   2.2740      0.00    -0.37       0.00    -0.05
    12   2.2741      0.00    -0.40       0.00    -0.16
    13   4.1334      0.00    -0.26       0.00    -0.54
    14   4.1337      0.00    -0.31       0.00     0.62
    15   6.9265      0.00    -0.43       0.00     0.85
    16   6.9265      0.00    -0.44       0.00     0.88
    17   6.9266      0.00    -0.39       0.00     0.83
    18   6.9267      0.00    -0.40       0.00     0.86
    19   7.2246      0.00     0.51       0.00    -0.48
    20   7.2246      0.00     0.42       0.00    -0.45
    21   7.2246      0.00     0.43       0.00    -0.47
    22   8.3285      0.00     0.01       0.00    -0.08
    23   8.3285      0.00     0.07       0.00    -0.12
    24   8.3286      0.00     0.05       0.00    -0.11
    25   8.3286      0.00    -0.04       0.00    -0.06
    26   8.3286      0.00     0.09       0.00     0.26
    27   8.3287      0.00    -0.08       0.00     0.28
    28   8.3287      0.00     0.07       0.00     0.32
    29   8.3287      0.00     0.06       0.00     0.35
    30  17.0890      0.00     0.20       0.00    -0.38
    31  17.0892      0.00     0.11       0.00    -0.16
    32  17.0893      0.00     0.23       0.00    -0.26
    33  19.3252      0.00    -0.32       0.00    -0.03
    34  19.3254      0.00     0.02       0.00    -0.07

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.

01PK47    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        40.090    40.089    40.090
ecceobj         0.071     0.071     0.071
incobj          8.719     8.719     8.719
qmin           35.710    35.708    35.681
qmax           44.209    44.209    44.173
amean          39.809    39.809    39.809
amin           39.463    39.467    39.465
amax           40.172    40.168    40.172
emean           0.063     0.063     0.064
emin            0.020     0.020     0.020
emax            0.101     0.101     0.101
imean          12.430    12.430    12.430
imin            8.756     8.756     8.754
imax           14.595    14.591    14.595
excite_mean     0.225     0.225     0.225
fracstop        1.000     1.000     1.000
cjmean          2.994     2.994     2.994

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       179.8     179.9     179.8
kozaiamp        180.0     180.0     180.0