Orbit Fit and Astrometric record for 620088

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: 620088    
# Created Sun Nov 24 02:07:45 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     64 observations of     64
# Arc:  21.09y
# First observation: 2002/02/13
#  Last observation: 2023/03/18
# Chi-squared of fit:    75.09 DOF:    122 RMS:  0.19
# Min/Max residuals:    -0.52    0.41
# Exact a, adot, b, bdot, g, gdot:
  1.694616E-05  2.756133E-02 -6.417553E-07  2.927080E-04  2.535586E-02 -2.282959E-03
# Covariance matrix:
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
#      lat0       lon0       xBary       yBary       zBary        JD0
  -13.073592  133.282266   -0.193968   -0.218562   -0.940817  2452318.754200
# Heliocentric elements and errors
Epoch:              2452318.5000  =  2002/02/13
Mean Anomaly:          345.81654 +/-     0.000
Argument of Peri:      296.44380 +/-     0.000
Long of Asc Node:      220.30283 +/-     0.000
Inclination:            12.78240 +/-     0.000
Eccentricity:         0.23422056 +/-    0.0000
Semi-Major Axis:     51.92136462 +/-    0.0000
Time of Perihelion: 2457702.4032 +/-       0.0
Perihelion:          39.76031340 +/-    0.0000
Aphelion:            64.08241584 +/-    0.0000
Period (y)              374.1341 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -27.14071088 +/-    0.0000
Ecliptic Y           28.54180559 +/-    0.0000
Ecliptic Z           -8.92112267 +/-    0.0000
Ecliptic XDOT        -0.00201524 +/-    0.0000
Ecliptic YDOT        -0.00221067 +/-    0.0000
Ecliptic ZDOT         0.00008676 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   40.38370277 +/-    0.0000
Geocenter to KBO     39.43870323 +/-    0.0000
# Hcoef:  6.60

The following table shows the complete astrometric record for 620088. 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 (620088) followed by the observatory code and reference code for the source of the astrometry.

2002 02  13.253457 08 48 10.27   +04 16 27.9   22.5r 620088    645  C~444E      
2002 02  13.254287 08 48 10.28   +04 16 27.8   22.1i 620088    645  C~444E      
2002 02  13.255945 08 48 10.24   +04 16 27.8   21.6z 620088    645  C~444E      
2002 02  13.256775 08 48 10.27   +04 16 27.8   23.5g 620088    645  C~444E      
2006 11  18.449231 09 23 34.50   +02 03 02.4   22.5r 620088    645  C~444E      
2006 11  18.450060 09 23 34.49   +02 03 02.4   22.0i 620088    645  C~444E      
2006 11  18.452548 09 23 34.48   +02 03 02.1         620088    645  C~444E      
2007 03  14.228430 09 16 55.61   +02 21 33.7   22.2r 620088    645  C~444E      
2007 03  14.229259 09 16 55.60   +02 21 33.6   22.0i 620088    645  C~444E      
2007 03  14.230918 09 16 55.59   +02 21 33.6   21.3z 620088    645  C~444E      
2007 03  14.231747 09 16 55.59   +02 21 33.4   23.6g 620088    645  C~444E      
2015 02  17.15003  10 08 42.59   -01 23 14.5   23.5g 620088    W84  C~2iOW      
2015 02  17.23580  10 08 42.19   -01 23 12.2   23.3g 620088    W84  C~2iOW      
2015 02  17.30445  10 08 41.86   -01 23 10.5   23.4g 620088    W84  C~2iOW      
2015 02  17.35153  10 08 41.64   -01 23 09.2   23.7g 620088    W84  C~2iOW      
2015 02  18.07910  10 08 38.20   -01 22 49.9   23.1g 620088    W84  C~2iOW      
2015 02  18.14658  10 08 37.86   -01 22 47.9   23.4g 620088    W84  C~2iOW      
2015 02  18.21462  10 08 37.55   -01 22 46.2   23.4g 620088    W84  C~2iOW      
2015 02  18.28477  10 08 37.20   -01 22 44.2         620088    W84  C~2iOW      
2015 02  18.35376  10 08 36.89   -01 22 42.6   23.6g 620088    W84  C~2iOW      
2015 02  19.07585  10 08 33.47   -01 22 23.3         620088    W84  C~2iOW      
2015 02  19.07635  10 08 33.46   -01 22 22.7   23.7g 620088    W84  C~2y2b      
2015 02  19.14370  10 08 33.15   -01 22 20.7         620088    W84  C~2y2b      
2015 02  19.21297  10 08 32.80   -01 22 19.3   23.6g 620088    W84  C~2iOW      
2015 02  19.21347  10 08 32.79   -01 22 18.9         620088    W84  C~2y2b      
2015 02  19.28175  10 08 32.47   -01 22 17.6   23.5g 620088    W84  C~2iOW      
2015 02  19.28225  10 08 32.47   -01 22 17.0         620088    W84  C~2y2b      
2015 02  19.35086  10 08 32.13   -01 22 15.9         620088    W84  C~2iOW      
2015 02  22.06830  10 08 19.28   -01 21 00.7         620088    W84  C~2iOW      
2015 02  22.13567  10 08 18.94   -01 20 58.7         620088    W84  C~2iOW      
2015 02  22.27270  10 08 18.30   -01 20 55.0         620088    W84  C~2iOW      
2015 02  22.34137  10 08 17.95   -01 20 53.0         620088    W84  C~2iOW      
2015 02  24.053484 10 08 09.86   -01 20 03.9   22.6r 620088    W84  C~444E      
2015 02  27.054086 10 07 55.72   -01 18 36.6         620088    W84  C~444E      
2015 03  08.239514 10 07 13.49   -01 13 55.4   22.3r 620088    W84  C~444E      
2015 03  19.006331 10 06 27.34   -01 08 07.3   21.9i 620088    W84  C~444E      
2015 03  23.115706 10 06 11.10   -01 05 52.3   23.3g 620088    W84  C~444E      
2015 04  09.064334 10 05 14.92   -00 56 46.5   21.9z 620088    W84  C~444E      
2015 05  17.001845 10 04 32.66   -00 40 58.8   22.7r 620088    309  C~444E      
2015 05  17.005829 10 04 32.67   -00 40 58.9   22.6r 620088    309  C~444E      
2015 05  17.009829 10 04 32.65   -00 40 58.8   22.3r 620088    309  C~444E      
2015 05  17.013814 10 04 32.68   -00 40 58.8   22.5r 620088    309  C~444E      
2015 05  17.054774 10 04 32.68   -00 40 57.7         620088    309  C~444E      
2015 05  17.058759 10 04 32.66   -00 40 57.9         620088    309  C~444E      
2015 05  17.062744 10 04 32.69   -00 40 57.8   23.5g 620088    309  C~444E      
2015 05  17.066729 10 04 32.70   -00 40 58.0         620088    309  C~444E      
2015 05  18.015311 10 04 33.34   -00 40 42.0   23.7g 620088    309  C~444E      
2015 05  18.019294 10 04 33.35   -00 40 41.7   23.7g 620088    309  C~444E      
2015 05  18.023276 10 04 33.34   -00 40 41.9         620088    309  C~444E      
2015 05  18.027261 10 04 33.34   -00 40 41.8         620088    309  C~444E      
2016 01  16.288125 10 17 18.43   -01 59 52.4   22.4r 620088    W84  C~444E      
2016 01  16.289115 10 17 18.45   -01 59 52.2   22.7g 620088    W84  C~444E      
2016 02  28.278715 10 14 09.40   -01 44 59.8   21.9z 620088    W84  C~444E      
2016 12  29.322633 10 24 23.19   -02 27 20.4   23.4g 620088    W84  C~444E      
2017 03  04.124485 10 20 06.40   -02 09 29.9   23.3g 620088    W84  C~444E      
2017 03  30.993113 10 18 14.21   -01 54 50.1   21.8z 620088    W84  C~444E      
2018 02  07.382604 10 28 20.97   -02 47 20.7   21.7z 620088    W84  C~444E      
2018 02  08.329473 10 28 16.74   -02 47 00.2   21.7z 620088    W84  C~444E      
2023 01  22.509031 11 00 44.707  -05 01 29.49  22.4w 620088    F52  C~6mw2      
2023 01  22.521748 11 00 44.676  -05 01 29.54  22.5w 620088    F52  C~6mw2      
2023 01  22.534525 11 00 44.617  -05 01 28.99  22.6w 620088    F52  C~6mw2      
2023 03  18.276400 10 56 50.748  -04 39 51.26  22.6G 620088    G37  C~6VBC      
2023 03  18.320180 10 56 50.557  -04 39 50.32        620088    G37  C~6VBC      
2023 03  18.362600 10 56 50.389  -04 39 48.25        620088    G37  C~6VBC      

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     0.15
     2   0.0000      0.00     0.30       0.00     0.03
     3   0.0000      0.00    -0.18       0.00    -0.01
     4   0.0000      0.00     0.33       0.00    -0.03
     5   4.7617      0.00    -0.00       0.00     0.20
     6   4.7617      0.00    -0.16       0.00     0.22
     7   4.7617      0.00    -0.31       0.00    -0.03
     8   5.0786      0.00    -0.05       0.00     0.16
     9   5.0786      0.00    -0.16       0.00     0.04
    10   5.0787      0.00    -0.21       0.00    -0.01
    11   5.0787      0.00    -0.17       0.00    -0.23
    12  13.0100      0.00    -0.08       0.00    -0.21
    13  13.0102      0.00     0.12       0.00    -0.17
    14  13.0104      0.00     0.14       0.00    -0.28
    15  13.0105      0.00     0.23       0.00    -0.22
    16  13.0125      0.00     0.11       0.00    -0.22
    17  13.0127      0.00    -0.12       0.00    -0.02
    18  13.0129      0.00     0.16       0.00    -0.13
    19  13.0131      0.00    -0.02       0.00    -0.01
    20  13.0133      0.00     0.31       0.00    -0.26
    21  13.0153      0.00     0.12       0.00    -0.38
    22  13.0153      0.00     0.01       0.00     0.21
    23  13.0154      0.00     0.22       0.00     0.39
    24  13.0156      0.00    -0.01       0.00    -0.09
    25  13.0156      0.00    -0.13       0.00     0.30
    26  13.0158      0.00     0.02       0.00    -0.25
    27  13.0158      0.00     0.05       0.00     0.34
    28  13.0160      0.00    -0.10       0.00    -0.43
    29  13.0234      0.00     0.26       0.00    -0.24
    30  13.0236      0.00     0.02       0.00    -0.13
    31  13.0240      0.00     0.32       0.00    -0.28
    32  13.0242      0.00     0.02       0.00    -0.22
    33  13.0289      0.00    -0.10       0.00     0.20
    34  13.0371      0.00    -0.26       0.00     0.06
    35  13.0622      0.00    -0.03       0.00    -0.40
    36  13.0917      0.00    -0.30       0.00    -0.00
    37  13.1030      0.00    -0.07       0.00     0.17
    38  13.1494      0.00    -0.12       0.00     0.41
    39  13.2532      0.00    -0.06       0.00     0.12
    40  13.2533      0.00     0.05       0.00    -0.05
    41  13.2533      0.00    -0.28       0.00    -0.01
    42  13.2533      0.00     0.14       0.00    -0.08
    43  13.2534      0.00    -0.19       0.00     0.32
    44  13.2534      0.00    -0.52       0.00     0.06
    45  13.2534      0.00    -0.11       0.00     0.09
    46  13.2534      0.00     0.01       0.00    -0.18
    47  13.2560      0.00     0.11       0.00    -0.04
    48  13.2560      0.00     0.22       0.00     0.19
    49  13.2560      0.00     0.03       0.00    -0.07
    50  13.2561      0.00    -0.00       0.00    -0.04
    51  13.9221      0.00    -0.09       0.00     0.07
    52  13.9221      0.00     0.26       0.00     0.27
    53  14.0398      0.00     0.02       0.00     0.21
    54  14.8749      0.00     0.04       0.00    -0.00
    55  15.0524      0.00    -0.10       0.00     0.14
    56  15.1259      0.00     0.05       0.00    -0.03
    57  15.9839      0.00    -0.02       0.00     0.04
    58  15.9865      0.00    -0.06       0.00     0.18
    59  20.9398      0.00    -0.10       0.00     0.11
    60  20.9398      0.00     0.06       0.00    -0.06
    61  20.9399      0.00    -0.20       0.00     0.37
    62  21.0897      0.00    -0.17       0.00     0.11
    63  21.0898      0.00    -0.03       0.00    -0.42
    64  21.0900      0.00     0.35       0.00     0.23

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.

620088    quality flag:3

Type:       SCATNEAR  SCATNEAR  SCATNEAR

axisobj        51.485    51.485    51.486
ecceobj         0.228     0.228     0.228
incobj         12.783    12.783    12.783
qmin           39.145    39.149    39.105
qmax           64.537    64.532    64.393
amean          51.528    51.528    51.529
amin           51.056    51.051    51.045
amax           52.111    52.094    52.093
emean           0.225     0.225     0.225
emin            0.213     0.213     0.212
emax            0.238     0.239     0.237
imean          13.752    13.752    13.752
imin           13.330    13.333    13.333
imax           14.115    14.115    14.114
excite_mean     0.327     0.327     0.327
fracstop        1.000     1.000     1.000
cjmean          3.060     3.060     3.060

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       174.4     174.5     174.5
kozaiamp        180.0     180.0     180.0