Orbit Fit and Astrometric record for 15RC280

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: 15RC280   
# Created Sun Nov 24 02:10:25 2024
# Orbit generated from Bernstein formalism
# Fitting     23 observations of     23
# Arc:   2.36y
# First observation: 2015/07/14
#  Last observation: 2017/11/22
Preliminary a, adot, b, bdot, g, gdot:
  -0.000115   0.024584   0.000001   0.000150   0.024478   0.000000
# Chi-squared of fit:     5.12 DOF:     40 RMS:  0.08
# Min/Max residuals:    -0.15    0.23
# Exact a, adot, b, bdot, g, gdot:
  1.571733E-05  2.426388E-02  2.091120E-07  1.492655E-04  2.430047E-02  9.573787E-04
# Covariance matrix:
  2.7904E-13  8.9035E-14 -1.2342E-15  2.4617E-15  2.7106E-13  6.8579E-12
  8.9035E-14  5.6906E-13 -2.6709E-15  7.7062E-15  4.5827E-13  2.2662E-11
 -1.2342E-15 -2.6709E-15  1.2503E-13 -9.8916E-14 -2.9816E-15 -1.4567E-13
  2.4617E-15  7.7062E-15 -9.8916E-14  1.5636E-13  7.6000E-15  4.7574E-13
  2.7106E-13  4.5827E-13 -2.9816E-15  7.6000E-15  5.6567E-13  2.2002E-11
  6.8579E-12  2.2662E-11 -1.4567E-13  4.7574E-13  2.2002E-11  1.4183E-09
#      lat0       lon0       xBary       yBary       zBary        JD0
    0.290981   10.989124    0.999535    0.001071   -0.190727  2457218.072199
# Heliocentric elements and errors
Epoch:              2457210.5000  =  2015/07/07
Mean Anomaly:           17.92764 +/-     1.790
Argument of Peri:       19.10309 +/-     1.970
Long of Asc Node:      330.91630 +/-     0.074
Inclination:             0.46338 +/-     0.001
Eccentricity:         0.04383154 +/-    0.0006
Semi-Major Axis:     43.14126458 +/-    0.0047
Time of Perihelion: 2452056.3333 +/-     514.6
Perihelion:          41.25031661 +/-    0.0261
Aphelion:            45.03221256 +/-    0.0262
Period (y)              283.3658 +/-      0.05
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           40.77054270 +/-    0.0013
Ecliptic Y            6.89980116 +/-    0.0002
Ecliptic Z            0.20904983 +/-    0.0000
Ecliptic XDOT        -0.00041759 +/-    0.0000
Ecliptic YDOT         0.00269786 +/-    0.0000
Ecliptic ZDOT         0.00001743 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   41.35079334 +/-    0.0012
Geocenter to KBO     41.15145952 +/-    0.0013
# Hcoef:  8.84

The following table shows the complete astrometric record for 15RC280. 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 (15RC280) followed by the observatory code and reference code for the source of the astrometry.

2015 07  14.57141  00 39 56.997  +04 36 58.96  25.2r 15RC280   568  C~2nvp      
2015 07  19.54942  00 39 55.198  +04 36 50.34  25.0r 15RC280   568  C~2nvp      
2015 09  08.40906  00 37 48.086  +04 23 42.93  24.9r 15RC280   568  C~2nvp      
2015 09  08.51318  00 37 47.665  +04 23 40.51  24.6r 15RC280   568  C~2nvp      
2015 09  08.55681  00 37 47.479  +04 23 39.26  24.9r 15RC280   568  C~2nvp      
2015 09  09.53240  00 37 43.526  +04 23 14.31  25.3w 15RC280   568  C~2nvp      
2015 09  10.47324  00 37 39.681  +04 22 49.94  25.2w 15RC280   568  C~2nvp      
2015 09  16.46364  00 37 14.431  +04 20 10.45  23.3w 15RC280   568  C~2nvp      
2015 10  03.39174  00 35 58.858  +04 12 10.41  25.4w 15RC280   568  C~2nvp      
2015 10  07.35863  00 35 40.846  +04 10 15.73  24.4r 15RC280   568  C~2nvp      
2015 10  07.41176  00 35 40.598  +04 10 14.12  25.4r 15RC280   568  C~2nvp      
2015 11  07.25497  00 33 32.194  +03 56 30.00  25.7w 15RC280   568  C~2nvp      
2015 11  10.39374  00 33 21.336  +03 55 20.08  24.8w 15RC280   568  C~2nvp      
2015 12  07.33142  00 32 16.637  +03 48 17.18  25.1w 15RC280   568  C~2nvp      
2016 01  01.26036  00 32 11.712  +03 47 36.07  25.8w 15RC280   568  C~2nvp      
2016 09  05.53675  00 43 08.286  +04 58 13.54  25.4w 15RC280   568  C~2nvp      
2016 09  07.47613  00 43 00.669  +04 57 25.93  25.5w 15RC280   568  C~2nvp      
2016 09  07.52244  00 43 00.479  +04 57 24.76  25.3w 15RC280   568  C~2nvp      
2016 11  04.28299  00 38 51.216  +04 31 03.39  25.4w 15RC280   568  C~2nvp      
2016 11  04.34222  00 38 50.987  +04 31 02.03  25.4w 15RC280   568  C~2nvp      
2017 01  27.24379  00 38 10.674  +04 26 15.78  25.7w 15RC280   568  C~2nvp      
2017 01  28.23958  00 38 13.864  +04 26 35.87  25.6w 15RC280   568  C~2nvp      
2017 11  22.36455  00 43 03.663  +04 58 18.02  25.0w 15RC280   568  C~2nvp      

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     0.01       0.00    -0.02
     2   0.0136    -28.12     0.14       2.61     0.06
     3   0.1529  -2085.52    -0.10      23.55    -0.07
     4   0.1532  -2092.26     0.10      23.80     0.10
     5   0.1533  -2095.31    -0.04      23.74     0.01
     6   0.1560  -2159.49     0.01      23.99    -0.00
     7   0.1585  -2221.95     0.01      24.15    -0.07
     8   0.1749  -2631.95     0.01      25.70    -0.00
     9   0.2213  -3860.41    -0.12      28.28    -0.07
    10   0.2321  -4153.37    -0.02      28.73     0.09
    11   0.2323  -4157.41    -0.08      28.71     0.04
    12   0.3167  -6249.29     0.09      26.80    -0.06
    13   0.3253  -6426.35    -0.03      26.49     0.13
    14   0.3991  -7484.13     0.13      19.15    -0.10
    15   0.4673  -7568.19    -0.05      10.41    -0.07
    16   1.1471   3130.28    -0.07      54.36    -0.05
    17   1.1524   3006.87     0.03      55.01     0.05
    18   1.1525   3003.80    -0.00      55.04     0.05
    19   1.3106  -1044.26    -0.05      58.37    -0.13
    20   1.3108  -1047.94    -0.07      58.46    -0.06
    21   1.5405  -1714.79     0.23      31.59     0.09
    22   1.5432  -1663.02    -0.15      31.36     0.18
    23   2.3595   3068.43     0.04      85.48    -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.

15RC280    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        43.584    43.606    43.563
ecceobj         0.054     0.055     0.052
incobj          0.463     0.463     0.463
qmin           40.277    40.229    40.289
qmax           46.641    46.705    46.551
amean          43.343    43.366    43.323
amin           43.011    43.027    42.989
amax           43.695    43.719    43.673
emean           0.051     0.052     0.050
emin            0.031     0.033     0.030
emax            0.067     0.069     0.066
imean           2.174     2.177     2.170
imin            1.166     1.186     1.144
imax            2.927     2.921     2.929
excite_mean     0.064     0.065     0.063
fracstop        1.000     1.000     1.000
cjmean          3.089     3.089     3.089

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       183.8     184.6     183.6
kozaiamp        180.0     180.0     180.0