Orbit Fit and Astrometric record for 15HF195

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: 15HF195   
# Created Wed Dec 25 02:10:18 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     34 observations of     34
# Arc:   6.18y
# First observation: 2013/04/18
#  Last observation: 2019/06/23
# Chi-squared of fit:     4.61 DOF:     62 RMS:  0.07
# Min/Max residuals:    -0.11    0.16
# Exact a, adot, b, bdot, g, gdot:
  1.878538E-05  3.554723E-02  2.102025E-06  3.277955E-03  3.013482E-02  1.621495E-03
# Covariance matrix:
  2.8327E-13 -2.7854E-13  2.1163E-14 -2.6243E-14 -1.9975E-14 -1.2229E-12
 -2.7854E-13  3.3670E-13 -2.6854E-14  3.3153E-14  4.5468E-14  1.5480E-12
  2.1163E-14 -2.6854E-14  9.4056E-14 -3.7893E-14 -1.5162E-15 -1.3534E-13
 -2.6243E-14  3.3153E-14 -3.7893E-14  2.9093E-14 -1.0212E-17  1.6848E-13
 -1.9975E-14  4.5468E-14 -1.5162E-15 -1.0212E-17  2.6017E-13  3.9029E-14
 -1.2229E-12  1.5480E-12 -1.3534E-13  1.6848E-13  3.9029E-14  7.8375E-12
#      lat0       lon0       xBary       yBary       zBary        JD0
   -3.283167 -151.383331    0.007920   -0.057547   -1.004206  2456400.616530
# Heliocentric elements and errors
Epoch:              2456400.5000  =  2013/04/18
Mean Anomaly:            9.38375 +/-     0.013
Argument of Peri:      313.81039 +/-     0.022
Long of Asc Node:      239.64638 +/-     0.001
Inclination:             6.16167 +/-     0.000
Eccentricity:         0.22037311 +/-    0.0001
Semi-Major Axis:     43.58035618 +/-    0.0046
Time of Perihelion: 2453661.3965 +/-       3.9
Perihelion:          33.97641733 +/-    0.0051
Aphelion:            53.18429502 +/-    0.0067
Period (y)              287.7030 +/-      0.05
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -29.96859481 +/-    0.0005
Ecliptic Y          -16.34020481 +/-    0.0003
Ecliptic Z           -1.90041556 +/-    0.0000
Ecliptic XDOT         0.00139641 +/-    0.0000
Ecliptic YDOT        -0.00291342 +/-    0.0000
Ecliptic ZDOT         0.00028903 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   34.18667225 +/-    0.0004
Geocenter to KBO     33.18421260 +/-    0.0006
# Hcoef:  7.23

The following table shows the complete astrometric record for 15HF195. 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 (15HF195) followed by the observatory code and reference code for the source of the astrometry.

2013 04  18.115752 13 41 33.14   -14 02 55.3         15HF195   W84  C~55Q0      
2013 04  18.119919 13 41 33.13   -14 02 55.2         15HF195   W84  C~55Q0      
2013 04  18.124063 13 41 33.09   -14 02 55.0         15HF195   W84  C~55Q0      
2013 04  18.128252 13 41 33.08   -14 02 54.9         15HF195   W84  C~55Q0      
2014 03  28.23828  13 51 32.57   -14 46 13.6         15HF195   W84  C~55Q0      
2014 03  28.30106  13 51 32.26   -14 46 11.9   22.7V 15HF195   W84  C~55Q0      
2014 03  28.38479  13 51 31.83   -14 46 09.7         15HF195   W84  C~55Q0      
2014 04  23.097720 13 49 14.09   -14 33 15.4         15HF195   W84  C~55Q0      
2014 04  23.100984 13 49 14.07   -14 33 15.3         15HF195   W84  C~55Q0      
2014 04  23.104213 13 49 14.05   -14 33 15.2         15HF195   W84  C~55Q0      
2014 04  23.107454 13 49 14.03   -14 33 15.0         15HF195   W84  C~55Q0      
2014 04  23.110694 13 49 14.01   -14 33 14.9         15HF195   W84  C~55Q0      
2014 04  24.117859 13 49 08.48   -14 32 42.4         15HF195   W84  C~55Q0      
2014 04  24.121111 13 49 08.46   -14 32 42.3         15HF195   W84  C~55Q0      
2014 04  24.124363 13 49 08.44   -14 32 42.2         15HF195   W84  C~55Q0      
2014 04  24.127593 13 49 08.43   -14 32 42.1         15HF195   W84  C~55Q0      
2014 04  24.130822 13 49 08.41   -14 32 42.0         15HF195   W84  C~55Q0      
2014 04  25.117025 13 49 02.99   -14 32 09.9         15HF195   W84  C~55Q0      
2014 04  25.120278 13 49 02.98   -14 32 09.9         15HF195   W84  C~55Q0      
2014 04  25.123507 13 49 02.96   -14 32 09.8         15HF195   W84  C~55Q0      
2014 04  25.126759 13 49 02.94   -14 32 09.6         15HF195   W84  C~55Q0      
2014 04  25.130000 13 49 02.92   -14 32 09.5         15HF195   W84  C~55Q0      
2014 06  27.965463 13 44 57.18   -14 03 56.9         15HF195   W84  C~55Q0      
2014 06  28.111412 13 44 56.99   -14 03 54.8         15HF195   W84  C~55Q0      
2014 06  28.988472 13 44 55.99   -14 03 42.9         15HF195   W84  C~55Q0      
2014 06  28.989630 13 44 55.99   -14 03 42.9         15HF195   W84  C~55Q0      
2015 01  31.288310 14 02 03.68   -15 28 02.4         15HF195   W84  C~55Q0      
2015 01  31.290370 14 02 03.68   -15 28 02.2         15HF195   W84  C~55Q0      
2015 04  25.02502  13 57 12.76   -15 04 10.8   22.5V 15HF195   W84  C~2gaG      
2015 04  25.09398  13 57 12.37   -15 04 08.7         15HF195   W84  C~2gaG      
2015 04  26.08949  13 57 06.89   -15 03 37.0         15HF195   W84  C~2gaG      
2015 04  26.15834  13 57 06.50   -15 03 34.9         15HF195   W84  C~2gaG      
2019 06  23.052465 14 25 10.33   -16 33 28.3         15HF195   W84  C~55Q0      
2019 06  23.101591 14 25 10.18   -16 33 27.3         15HF195   W84  C~55Q0      

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    -0.06
     2   0.0000      0.00     0.14       0.00    -0.10
     3   0.0000      0.00    -0.11       0.00    -0.03
     4   0.0000      0.00     0.09       0.00    -0.07
     5   0.9422      0.00    -0.08       0.00     0.05
     6   0.9423      0.00     0.05       0.00     0.08
     7   0.9426      0.00    -0.04       0.00     0.03
     8   1.0130      0.00     0.02       0.00    -0.00
     9   1.0130      0.00    -0.01       0.00    -0.01
    10   1.0130      0.00    -0.03       0.00    -0.01
    11   1.0130      0.00    -0.06       0.00     0.09
    12   1.0130      0.00    -0.09       0.00     0.08
    13   1.0157      0.00     0.01       0.00    -0.05
    14   1.0158      0.00    -0.02       0.00    -0.05
    15   1.0158      0.00    -0.04       0.00    -0.06
    16   1.0158      0.00     0.08       0.00    -0.06
    17   1.0158      0.00     0.05       0.00    -0.07
    18   1.0185      0.00    -0.09       0.00     0.01
    19   1.0185      0.00     0.03       0.00    -0.09
    20   1.0185      0.00     0.00       0.00    -0.10
    21   1.0185      0.00    -0.03       0.00    -0.00
    22   1.0185      0.00    -0.05       0.00    -0.01
    23   1.1933      0.00     0.04       0.00     0.11
    24   1.1937      0.00     0.03       0.00     0.16
    25   1.1961      0.00    -0.02       0.00     0.07
    26   1.1961      0.00     0.00       0.00     0.06
    27   1.7883      0.00    -0.01       0.00    -0.06
    28   1.7883      0.00    -0.02       0.00     0.16
    29   2.0175      0.00     0.07       0.00     0.04
    30   2.0177      0.00    -0.01       0.00    -0.03
    31   2.0205      0.00     0.11       0.00     0.05
    32   2.0207      0.00     0.05       0.00    -0.03
    33   6.1792      0.00     0.03       0.00    -0.07
    34   6.1793      0.00    -0.07       0.00    -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.

15HF195    quality flag:3

Type:       SCATNEAR  SCATNEAR  SCATNEAR

axisobj        43.366    43.366    43.366
ecceobj         0.216     0.216     0.216
incobj          6.161     6.161     6.161
qmin           32.644    32.643    32.644
qmax           55.225    55.223    55.229
amean          43.726    43.726    43.726
amin           43.294    43.293    43.297
amax           44.212    44.214    44.214
emean           0.193     0.193     0.193
emin            0.068     0.067     0.068
emax            0.251     0.251     0.251
imean           9.121     9.117     9.120
imin            5.429     5.427     5.430
imax           14.841    14.846    14.850
excite_mean     0.260     0.260     0.260
fracstop        1.000     1.000     1.000
cjmean          3.016     3.016     3.016

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       251.9     252.2     252.2
kozaiamp         69.9      69.8      68.9