Orbit Fit and Astrometric record for 15RA280

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: 15RA280   
# Created Sun Nov 24 02:10:25 2024
# Orbit generated from Bernstein formalism
# Fitting     34 observations of     34
# Arc:   2.50y
# First observation: 2015/06/23
#  Last observation: 2017/12/23
Preliminary a, adot, b, bdot, g, gdot:
  -0.000061   0.017667   0.000002   0.000575   0.020598   0.000000
# Chi-squared of fit:     7.50 DOF:     62 RMS:  0.08
# Min/Max residuals:    -0.30    0.22
# Exact a, adot, b, bdot, g, gdot:
  1.358041E-05  1.732576E-02  1.167877E-06  5.680852E-04  2.031260E-02  6.597022E-04
# Covariance matrix:
  1.7828E-13  2.9363E-14 -2.3048E-15  4.3477E-15  1.5221E-13  2.9474E-12
  2.9363E-14  2.5259E-13 -4.9998E-15  1.2415E-14  2.4040E-13  8.4827E-12
 -2.3048E-15 -4.9998E-15  9.8660E-14 -6.1677E-14 -6.3284E-15 -2.3230E-13
  4.3477E-15  1.2415E-14 -6.1677E-14  6.7393E-14  1.4358E-14  6.2274E-13
  1.5221E-13  2.4040E-13 -6.3284E-15  1.4358E-14  3.4508E-13  9.7876E-12
  2.9474E-12  8.4827E-12 -2.3230E-13  6.2274E-13  9.7876E-12  4.2626E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
    0.552195   10.741943    1.004019   -0.001422    0.157677  2457197.114678
# Heliocentric elements and errors
Epoch:              2457190.5000  =  2015/06/17
Mean Anomaly:          169.70103 +/-     0.615
Argument of Peri:      204.77201 +/-     0.617
Long of Asc Node:      353.28198 +/-     0.007
Inclination:             1.97452 +/-     0.001
Eccentricity:         0.09901178 +/-    0.0001
Semi-Major Axis:     44.71162670 +/-    0.0027
Time of Perihelion: 2514915.3849 +/-     186.5
Perihelion:          40.28464886 +/-    0.0068
Aphelion:            49.13860454 +/-    0.0070
Period (y)              298.9778 +/-      0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           48.39428098 +/-    0.0014
Ecliptic Y            8.16013879 +/-    0.0003
Ecliptic Z            0.47456900 +/-    0.0000
Ecliptic XDOT        -0.00035109 +/-    0.0000
Ecliptic YDOT         0.00230454 +/-    0.0000
Ecliptic ZDOT         0.00007749 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   49.07972609 +/-    0.0014
Geocenter to KBO     49.23053350 +/-    0.0014
# Hcoef:  7.55

The following table shows the complete astrometric record for 15RA280. 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 (15RA280) followed by the observatory code and reference code for the source of the astrometry.

2015 06  23.61390  00 38 37.584  +04 45 35.31  23.9r 15RA280   568  C~2nvo      
2015 07  14.54595  00 38 48.370  +04 47 07.06  24.6r 15RA280   568  C~2nvo      
2015 07  19.51084  00 38 46.202  +04 46 58.70  24.7r 15RA280   568  C~2nvo      
2015 08  11.50339  00 38 13.754  +04 43 55.66  26.4r 15RA280   568  C~2nvo      
2015 08  11.54506  00 38 13.629  +04 43 55.09  26.1r 15RA280   568  C~2nvo      
2015 09  08.40906  00 36 52.864  +04 35 43.05  24.3r 15RA280   568  C~2nvo      
2015 09  08.51318  00 36 52.495  +04 35 40.88  24.4r 15RA280   568  C~2nvo      
2015 09  08.55681  00 36 52.328  +04 35 39.88  25.5r 15RA280   568  C~2nvo      
2015 09  09.53240  00 36 48.896  +04 35 18.54  24.6w 15RA280   568  C~2nvo      
2015 09  10.47324  00 36 45.552  +04 34 57.82  24.7w 15RA280   568  C~2nvo      
2015 09  16.46364  00 36 23.640  +04 32 41.78  25.2w 15RA280   568  C~2nvo      
2015 10  03.39174  00 35 18.297  +04 25 51.89  24.4w 15RA280   568  C~2nvo      
2015 10  07.35864  00 35 02.710  +04 24 13.72  24.8r 15RA280   568  C~2nvo      
2015 11  07.25497  00 33 11.336  +04 12 23.36  24.6w 15RA280   568  C~2nvo      
2015 11  07.30781  00 33 11.168  +04 12 22.28  25.0w 15RA280   568  C~2nvo      
2015 11  10.39374  00 33 01.889  +04 11 22.43  25.1w 15RA280   568  C~2nvo      
2015 12  07.33142  00 32 04.597  +04 05 07.79  20.4w 15RA280   568  C~2nvo      
2016 01  01.26036  00 31 57.831  +04 04 13.85  25.0w 15RA280   568  C~2nvo      
2016 09  05.53675  00 40 41.174  +05 02 06.24  23.8w 15RA280   568  C~2nvo      
2016 09  07.47613  00 40 34.510  +05 01 25.36  24.5w 15RA280   568  C~2nvo      
2016 09  07.52244  00 40 34.351  +05 01 24.39  24.7w 15RA280   568  C~2nvp      
2016 09  27.48878  00 39 19.847  +04 53 41.86  24.8w 15RA280   568  C~2nvp      
2016 11  04.28299  00 36 58.775  +04 38 48.52  25.3w 15RA280   568  C~2nvp      
2016 11  04.34222  00 36 58.576  +04 38 47.39  24.7w 15RA280   568  C~2nvp      
2016 12  29.26158  00 35 33.185  +04 29 22.30  24.7w 15RA280   568  C~2nvp      
2017 01  03.23211  00 35 36.382  +04 29 40.28  24.9w 15RA280   568  C~2nvp      
2017 01  27.23800  00 36 18.351  +04 33 57.50        15RA280   568  C~2nvp      
2017 01  28.23385  00 36 20.996  +04 34 14.25  24.3w 15RA280   568  C~2nvp      
2017 01  30.24057  00 36 26.500  +04 34 48.62  23.8w 15RA280   568  C~2nvp      
2017 09  16.50467  00 43 44.214  +05 23 44.50  24.8w 15RA280   568  C~2nvp      
2017 09  17.40380  00 43 40.883  +05 23 23.82  24.8w 15RA280   568  C~2nvp      
2017 09  22.45810  00 43 21.750  +05 21 25.52        15RA280   568  C~2nvp      
2017 11  22.37200  00 39 48.795  +04 58 57.81  24.7w 15RA280   568  C~2nvp      
2017 12  23.29716  00 39 09.385  +04 54 32.83  24.0w 15RA280   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    -0.02       0.00    -0.15
     2   0.0573    184.29     0.05      21.18    -0.07
     3   0.0709    151.20     0.02      26.20    -0.03
     4   0.1339   -366.77     0.15      48.06    -0.07
     5   0.1340   -368.71    -0.30      48.26     0.08
     6   0.2103  -1672.44     0.03      69.66    -0.00
     7   0.2105  -1678.36     0.11      69.83     0.06
     8   0.2107  -1681.05    -0.06      69.89     0.07
     9   0.2133  -1736.63     0.01      70.42    -0.00
    10   0.2159  -1790.75    -0.01      71.00     0.02
    11   0.2323  -2145.53    -0.09      74.60     0.14
    12   0.2787  -3205.31     0.22      81.78    -0.08
    13   0.2895  -3458.31    -0.09      83.19     0.12
    14   0.3741  -5270.16     0.06      85.85    -0.01
    15   0.3742  -5272.89     0.02      85.85    -0.03
    16   0.3827  -5424.16     0.04      85.52    -0.08
    17   0.4564  -6360.34    -0.08      78.95    -0.04
    18   0.5247  -6474.75    -0.03      69.28     0.01
    19   1.2044   2087.73     0.03     188.00    -0.03
    20   1.2098   1980.08    -0.01     189.37     0.07
    21   1.2099   1977.52     0.07     189.41     0.05
    22   1.2645    771.88    -0.00     199.95     0.02
    23   1.3680  -1518.31    -0.02     205.52    -0.06
    24   1.3682  -1521.49    -0.03     205.65     0.04
    25   1.5185  -2917.80    -0.01     187.71    -0.06
    26   1.5322  -2866.77    -0.06     185.45    -0.04
    27   1.5979  -2188.50    -0.01     175.31    -0.09
    28   1.6006  -2145.55     0.16     175.17     0.15
    29   1.6061  -2056.36    -0.14     174.45     0.13
    30   2.2338   5112.87    -0.01     314.19     0.02
    31   2.2362   5058.97     0.02     314.57    -0.07
    32   2.2501   4749.55    -0.06     317.21    -0.06
    33   2.4169   1293.71    -0.06     321.13     0.04
    34   2.5015    648.01     0.13     308.13    -0.05

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.

15RA280    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        45.125    45.135    45.117
ecceobj         0.089     0.089     0.089
incobj          1.964     1.964     1.964
qmin           39.862    39.874    39.839
qmax           50.206    50.233    50.175
amean          44.910    44.920    44.902
amin           44.543    44.557    44.538
amax           45.301    45.315    45.290
emean           0.094     0.094     0.094
emin            0.079     0.079     0.079
emax            0.108     0.109     0.109
imean           2.945     2.945     2.943
imin            2.244     2.247     2.241
imax            3.517     3.519     3.519
excite_mean     0.107     0.107     0.107
fracstop        1.000     1.000     1.000
cjmean          3.098     3.099     3.098

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       173.8     174.0     174.0
kozaiamp        180.0     180.0     179.9