Orbit Fit and Astrometric record for 15GU58

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: 15GU58    
# Created Sun Nov 24 02:10:18 2024
# Orbit generated from Bernstein formalism
# Fitting     36 observations of     36
# Arc:   2.35y
# First observation: 2015/02/17
#  Last observation: 2017/06/24
Preliminary a, adot, b, bdot, g, gdot:
  -0.000087   0.019265   0.000003  -0.000495   0.021532   0.000000
# Chi-squared of fit:     2.76 DOF:     66 RMS:  0.05
# Min/Max residuals:    -0.13    0.17
# Exact a, adot, b, bdot, g, gdot:
  1.377278E-05  1.915354E-02 -5.357331E-07 -4.920490E-04  2.155172E-02 -6.456906E-04
# Covariance matrix:
  1.6436E-13 -1.0726E-14 -5.3113E-16 -1.5876E-15  1.2048E-13  2.0742E-12
 -1.0726E-14  2.4028E-13  2.9588E-16 -5.9564E-15  1.5722E-13  7.5742E-12
 -5.3113E-16  2.9588E-16  8.9202E-14 -6.4305E-14 -4.4116E-16  2.0378E-14
 -1.5876E-15 -5.9564E-15 -6.4305E-14  8.4999E-14 -5.4794E-15 -2.9448E-13
  1.2048E-13  1.5722E-13 -4.4116E-16 -5.4794E-15  2.3652E-13  7.0323E-12
  2.0742E-12  7.5742E-12  2.0378E-14 -2.9448E-13  7.0323E-12  3.7394E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
    2.376575 -154.423011    0.828749    0.022236   -0.532431  2457071.093388
# Heliocentric elements and errors
Epoch:              2457070.5000  =  2015/02/17
Mean Anomaly:          223.60765 +/-     0.565
Argument of Peri:      263.28784 +/-     0.561
Long of Asc Node:       83.16246 +/-     0.015
Inclination:             2.75157 +/-     0.000
Eccentricity:         0.07477662 +/-    0.0006
Semi-Major Axis:     44.42775742 +/-    0.0044
Time of Perihelion: 2498050.0818 +/-     169.7
Perihelion:          41.10559968 +/-    0.0272
Aphelion:            47.74991516 +/-    0.0273
Period (y)              296.1350 +/-      0.04
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -42.65829650 +/-    0.0009
Ecliptic Y          -19.49724919 +/-    0.0004
Ecliptic Z            1.92405461 +/-    0.0000
Ecliptic XDOT         0.00111840 +/-    0.0000
Ecliptic YDOT        -0.00216606 +/-    0.0000
Ecliptic ZDOT        -0.00006576 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   46.94225146 +/-    0.0009
Geocenter to KBO     46.40000604 +/-    0.0010
# Hcoef:  6.73

The following table shows the complete astrometric record for 15GU58. 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 (15GU58) followed by the observatory code and reference code for the source of the astrometry.

2015 02  17.59261  13 38 19.423  -07 40 26.44  23.4r 15GU58    568  C~2nvb      
2015 02  17.63360  13 38 19.340  -07 40 25.91  23.2r 15GU58    568  C~2nvb      
2015 02  20.62674  13 38 13.492  -07 39 44.48  23.4r 15GU58    568  C~2nvb      
2015 03  18.57107  13 36 59.230  -07 31 43.52  23.3r 15GU58    568  C~2nvb      
2015 03  18.61845  13 36 59.059  -07 31 42.50  23.3r 15GU58    568  C~2nvb      
2015 03  20.57526  13 36 52.050  -07 30 59.22  23.3r 15GU58    568  C~2nvb      
2015 04  11.50958  13 35 25.833  -07 22 24.90  23.4r 15GU58    568  C~2nvb      
2015 04  13.37381  13 35 18.131  -07 21 40.21  23.4r 15GU58    568  C~2nvb      
2015 04  13.41479  13 35 17.959  -07 21 39.28  23.4r 15GU58    568  C~2nvb      
2015 04  13.51735  13 35 17.525  -07 21 36.82  23.4r 15GU58    568  C~2nvb      
2015 04  19.41451  13 34 53.126  -07 19 16.55  23.3r 15GU58    568  C~2nvb      
2015 04  19.53152  13 34 52.625  -07 19 13.78  23.2r 15GU58    568  C~2nvb      
2015 04  19.54875  13 34 52.553  -07 19 13.15  23.2r 15GU58    568  C~2nvb      
2015 05  18.33721  13 33 01.400  -07 09 02.76  23.4r 15GU58    568  C~2nvb      
2015 06  20.28725  13 31 39.238  -07 02 32.42  23.5r 15GU58    568  C~2nvb      
2015 06  20.32802  13 31 39.175  -07 02 32.21  23.5r 15GU58    568  C~2nvb      
2015 06  22.33199  13 31 36.465  -07 02 22.93  23.5r 15GU58    568  C~2nvb      
2015 07  14.28422  13 31 26.619  -07 02 41.35  23.4r 15GU58    568  C~2nvb      
2015 07  20.27721  13 31 30.442  -07 03 25.06  23.5r 15GU58    568  C~2nvb      
2016 02  04.58367  13 42 42.300  -08 08 03.13  23.7w 15GU58    568  C~2nvb      
2016 02  10.57151  13 42 36.473  -08 07 12.81  23.6w 15GU58    568  C~2nvb      
2016 02  10.61301  13 42 36.422  -08 07 12.43  23.7w 15GU58    568  C~2nvb      
2016 03  11.56297  13 41 28.119  -07 59 32.65  23.9w 15GU58    568  C~2nvb      
2016 04  03.45339  13 40 03.965  -07 51 04.43  23.6w 15GU58    568  C~2nvb      
2016 04  09.43453  13 39 39.586  -07 48 42.46  23.5w 15GU58    568  C~2nvb      
2016 05  01.46152  13 38 09.054  -07 40 12.46  23.6w 15GU58    568  C~2nvb      
2016 05  02.33557  13 38 05.592  -07 39 53.39  23.6w 15GU58    568  C~2nvb      
2016 05  07.33893  13 37 46.060  -07 38 07.44  23.3w 15GU58    568  C~2nvb      
2016 05  29.33959  13 36 31.186  -07 31 38.97  23.7w 15GU58    568  C~2nvb      
2016 06  04.40200  13 36 14.771  -07 30 19.98  23.6w 15GU58    568  C~2nvb      
2016 06  27.33817  13 35 34.457  -07 27 37.43  23.9w 15GU58    568  C~2nvb      
2016 07  07.32804  13 35 28.897  -07 27 39.54  23.8w 15GU58    568  C~2nvb      
2017 03  29.51368  13 44 33.936  -08 18 43.68  23.6w 15GU58    568  C~2nvb      
2017 03  30.48302  13 44 30.156  -08 18 21.53        15GU58    568  C~2nvb      
2017 03  30.48771  13 44 30.136  -08 18 21.39        15GU58    568  C~2nvb      
2017 06  24.30392  13 39 43.545  -07 53 15.34  23.9w 15GU58    568  C~2nvb      

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     0.06       0.00     0.04
     2   0.0001     -1.34     0.00       0.05    -0.00
     3   0.0083    -97.38     0.03       7.19    -0.01
     4   0.0793  -1300.80     0.02      55.28    -0.02
     5   0.0795  -1303.54     0.03      55.30    -0.04
     6   0.0848  -1416.37    -0.02      57.82     0.05
     7   0.1449  -2798.10     0.06      71.27     0.01
     8   0.1500  -2921.11    -0.10      71.24    -0.02
     9   0.1501  -2923.83    -0.07      71.17    -0.07
    10   0.1504  -2930.74    -0.10      71.12    -0.08
    11   0.1665  -3319.98     0.07      69.74     0.01
    12   0.1668  -3327.93    -0.05      69.61    -0.03
    13   0.1669  -3329.16    -0.13      69.80     0.17
    14   0.2457  -5092.62     0.02      35.60    -0.05
    15   0.3359  -6374.69     0.07     -47.64     0.01
    16   0.3360  -6375.64     0.04     -47.79    -0.00
    17   0.3415  -6416.62     0.04     -53.90     0.00
    18   0.4016  -6546.44    -0.03    -124.67     0.07
    19   0.4180  -6477.42     0.05    -144.55     0.02
    20   0.9637   4240.94    -0.04    -135.83     0.01
    21   0.9801   4142.07     0.01    -119.99    -0.00
    22   0.9802   4141.22     0.05    -119.91    -0.01
    23   1.0622   3028.95     0.04     -56.10    -0.04
    24   1.1249   1679.35     0.01     -33.05    -0.01
    25   1.1413   1290.24     0.02     -31.51     0.03
    26   1.2016   -148.75    -0.09     -42.78    -0.06
    27   1.2040   -203.62    -0.03     -43.64     0.00
    28   1.2176   -512.66     0.09     -50.08    -0.08
    29   1.2779  -1691.08     0.01     -91.82     0.00
    30   1.2945  -1947.23    -0.02    -106.86     0.01
    31   1.3573  -2564.95    -0.02    -173.26     0.03
    32   1.3846  -2641.23     0.00    -205.29     0.03
    33   2.1107   6018.85     0.00    -138.62     0.06
    34   2.1133   5958.48     0.01    -138.06    -0.03
    35   2.1133   5958.16    -0.01    -138.03    -0.00
    36   2.3483   1443.69    -0.02    -264.71     0.00

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.

15GU58    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        44.043    44.054    44.032
ecceobj         0.083     0.085     0.082
incobj          2.752     2.752     2.752
qmin           39.919    39.870    39.944
qmax           49.046    49.050    48.983
amean          44.326    44.339    44.318
amin           43.964    43.989    43.972
amax           44.708    44.714    44.704
emean           0.080     0.082     0.080
emin            0.065     0.065     0.064
emax            0.097     0.097     0.096
imean           1.080     1.078     1.084
imin            0.318     0.317     0.320
imax            1.623     1.623     1.633
excite_mean     0.083     0.084     0.082
fracstop        1.000     1.000     1.000
cjmean          3.097     3.097     3.097

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       178.5     178.4     177.2
kozaiamp        180.0     180.0     180.0