Orbit Fit and Astrometric record for 19UW173

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: 19UW173   
# Created Tue May  7 01:17:40 2024
# Orbit generated from Bernstein formalism
# Fitting     35 observations of     35
# Arc:  83.92d
# First observation: 2019/09/29
#  Last observation: 2019/12/22
Preliminary a, adot, b, bdot, g, gdot:
  -0.000068   0.034058   0.000056   0.006111   0.027870   0.000000
# Chi-squared of fit:    28.54 DOF:     64 RMS:  0.16
# Min/Max residuals:    -0.49    0.41
# Exact a, adot, b, bdot, g, gdot:
  1.592319E-05  2.805953E-02  4.885219E-06  6.691061E-03  2.701453E-02  3.182777E-03
# Covariance matrix:
  3.3326E-13 -2.9473E-12 -1.7376E-14  3.7990E-13  4.1924E-13  1.4375E-10
 -2.9473E-12  1.4405E-09  1.3354E-11 -1.3981E-10  2.0923E-10 -8.3552E-09
 -1.7376E-14  1.3354E-11  2.8620E-13 -2.3597E-12  1.9535E-12 -7.7744E-11
  3.7990E-13 -1.3981E-10 -2.3597E-12  2.3200E-11 -1.9638E-11  9.6925E-10
  4.1924E-13  2.0923E-10  1.9535E-12 -1.9638E-11  3.3452E-11 -6.7567E-10
  1.4375E-10 -8.3552E-09 -7.7744E-11  9.6925E-10 -6.7567E-10  1.5287E-07
#      lat0       lon0       xBary       yBary       zBary        JD0
  -17.262742   32.979830    0.450729   -0.264810   -0.852151  2458755.943631
# Heliocentric elements and errors
Epoch:              2458750.5000  =  2019/09/24
Mean Anomaly:           38.12952 +/-     2.602
Argument of Peri:      256.84336 +/-     4.028
Long of Asc Node:       83.30227 +/-     0.048
Inclination:            21.29285 +/-     0.013
Eccentricity:         0.14635101 +/-    0.0108
Semi-Major Axis:     42.32995874 +/-    0.1192
Time of Perihelion: 2448096.1001 +/-     725.8
Perihelion:          36.13492651 +/-    0.4664
Aphelion:            48.52499097 +/-    0.4752
Period (y)              275.4102 +/-      1.16
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           30.65012396 +/-    0.0063
Ecliptic Y           19.34294893 +/-    0.0041
Ecliptic Z          -10.98480324 +/-    0.0024
Ecliptic XDOT        -0.00111228 +/-    0.0000
Ecliptic YDOT         0.00266367 +/-    0.0000
Ecliptic ZDOT         0.00055162 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   37.87143612 +/-    0.0056
Geocenter to KBO     37.01711756 +/-    0.0079
# Hcoef:  9.65

The following table shows the complete astrometric record for 19UW173. 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 (19UW173) followed by the observatory code and reference code for the source of the astrometry.

2019 09  29.44283  02 26 24.44   -03 45 18.5   25.6r 19UW173   T09  C~7ulL      
2019 09  29.46532  02 26 24.34   -03 45 19.0   25.8r 19UW173   T09  C~7ulL      
2019 09  29.54579  02 26 23.97   -03 45 21.7   25.9i 19UW173   T09  C~7ulL      
2019 09  29.60928  02 26 23.71   -03 45 23.2   25.1z 19UW173   T09  C~7ulL      
2019 10  23.53309  02 24 29.84   -03 56 49.2   24.3z 19UW173   T09  C~7ulL      
2019 10  23.55512  02 24 29.73   -03 56 49.7   24.4z 19UW173   T09  C~7ulL      
2019 10  23.55861  02 24 29.71   -03 56 50.2   24.6z 19UW173   T09  C~7ulL      
2019 10  27.29097  02 24 10.46   -03 58 18.3   25.7r 19UW173   T09  C~7ulL      
2019 10  27.30213  02 24 10.39   -03 58 18.7   25.3r 19UW173   T09  C~7ulL      
2019 10  27.31332  02 24 10.33   -03 58 18.9   25.6r 19UW173   T09  C~7ulL      
2019 10  27.31576  02 24 10.32   -03 58 19.2   25.5r 19UW173   T09  C~7ulL      
2019 10  27.42875  02 24 09.73   -03 58 21.4   24.9i 19UW173   T09  C~7ulL      
2019 10  27.44703  02 24 09.62   -03 58 21.9   24.8i 19UW173   T09  C~7ulL      
2019 10  31.49580  02 23 48.57   -03 59 49.9   25.2z 19UW173   T09  C~7ulL      
2019 10  31.53991  02 23 48.32   -03 59 50.9   25.7z 19UW173   T09  C~7ulL      
2019 10  31.55809  02 23 48.24   -03 59 51.2   25.1z 19UW173   T09  C~7ulL      
2019 11  01.35808  02 23 44.06   -04 00 07.8   25.8g 19UW173   T09  C~7ulL      
2019 11  01.36928  02 23 44.03   -04 00 07.5   26.1g 19UW173   T09  C~7ulL      
2019 11  01.44979  02 23 43.59   -04 00 09.4   26.3g 19UW173   T09  C~7ulL      
2019 11  01.52871  02 23 43.18   -04 00 10.9   26.1g 19UW173   T09  C~7ulL      
2019 11  01.57346  02 23 42.95   -04 00 11.7   26.1g 19UW173   T09  C~7ulL      
2019 11  27.25481  02 21 35.18   -04 05 29.3   25.1z 19UW173   T09  C~7ulL      
2019 11  27.32148  02 21 34.89   -04 05 29.5   24.9i 19UW173   T09  C~7ulL      
2019 11  27.34361  02 21 34.76   -04 05 29.5   25.4i 19UW173   T09  C~7ulL      
2019 11  27.36574  02 21 34.67   -04 05 29.6   25.0i 19UW173   T09  C~7ulL      
2019 11  27.45540  02 21 34.27   -04 05 30.1   25.5r 19UW173   T09  C~7ulL      
2019 12  04.32949  02 21 04.44   -04 05 39.0   25.0z 19UW173   T09  C~7ulL      
2019 12  04.35162  02 21 04.36   -04 05 38.8   25.5z 19UW173   T09  C~7ulL      
2019 12  04.39987  02 21 04.15   -04 05 38.3   24.8i 19UW173   T09  C~7ulL      
2019 12  04.42190  02 21 04.07   -04 05 38.3   25.1i 19UW173   T09  C~7ulL      
2019 12  04.44386  02 21 03.97   -04 05 38.2   25.3i 19UW173   T09  C~7ulL      
2019 12  22.27977  02 20 01.65   -04 03 18.2   25.9r 19UW173   T09  C~7ulL      
2019 12  22.29498  02 20 01.61   -04 03 18.1   25.6r 19UW173   T09  C~7ulL      
2019 12  22.30453  02 20 01.57   -04 03 17.7   25.4r 19UW173   T09  C~7ulL      
2019 12  22.36184  02 20 01.43   -04 03 17.2   24.9i 19UW173   T09  C~7ulL      

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     0.10       0.00    -0.20
     2   0.0001     -1.58     0.13       0.03     0.02
     3   0.0003     -7.70    -0.25      -0.66    -0.01
     4   0.0005    -11.87     0.10      -0.78     0.41
     5   0.0660  -1847.38     0.10     -77.92     0.11
     6   0.0660  -1849.10     0.18     -77.84     0.12
     7   0.0660  -1849.55     0.02     -78.21    -0.26
     8   0.0762  -2150.52     0.15     -65.10    -0.01
     9   0.0763  -2151.64    -0.06     -65.13    -0.09
    10   0.0763  -2152.55    -0.06     -65.01    -0.03
    11   0.0763  -2152.80    -0.10     -65.25    -0.28
    12   0.0766  -2161.85     0.11     -64.37     0.05
    13   0.0767  -2163.57    -0.11     -64.30     0.04
    14   0.0878  -2489.91     0.05     -42.13    -0.06
    15   0.0879  -2493.77    -0.22     -41.83    -0.06
    16   0.0879  -2495.00     0.03     -41.71    -0.07
    17   0.0901  -2559.51    -0.49     -36.49    -0.15
    18   0.0901  -2559.83     0.10     -36.05     0.20
    19   0.0904  -2566.68    -0.18     -35.65     0.01
    20   0.0906  -2572.96    -0.04     -35.02     0.06
    21   0.0907  -2576.47     0.08     -34.62     0.12
    22   0.1610  -4485.34    -0.03     303.29    -0.00
    23   0.1612  -4489.50     0.25     304.55    -0.04
    24   0.1613  -4491.34    -0.11     305.19     0.18
    25   0.1613  -4492.64     0.06     305.55     0.10
    26   0.1616  -4498.45     0.20     307.07    -0.13
    27   0.1804  -4922.48    -0.23     447.33    -0.35
    28   0.1804  -4923.55     0.02     447.92    -0.26
    29   0.1806  -4926.35     0.08     449.43     0.18
    30   0.1806  -4927.47     0.25     449.83     0.09
    31   0.1807  -4928.85     0.16     450.43     0.20
    32   0.2295  -5762.15    -0.10     892.91     0.08
    33   0.2296  -5762.69    -0.08     893.20    -0.05
    34   0.2296  -5763.12    -0.17     893.78     0.26
    35   0.2298  -5764.93     0.07     894.95    -0.17

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.

19UW173    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        42.705    43.271    42.242
ecceobj         0.151     0.181     0.128
incobj         21.255    21.254    21.271
qmin           35.656    34.924    36.241
qmax           49.343    51.433    48.015
amean          42.328    42.982    41.966
amin           41.919    42.604    41.618
amax           42.742    43.416    42.336
emean           0.095     0.168     0.115
emin            0.024     0.150     0.098
emax            0.155     0.185     0.135
imean          20.386    19.723    19.638
imin           19.326    19.060    18.969
imax           21.365    20.444    20.312
excite_mean     0.363     0.377     0.355
fracstop        1.000     1.000     1.000
cjmean          2.923     2.919     2.927

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       268.5     180.6     178.2
kozaiamp         53.9     180.0     179.9