Orbit Fit and Astrometric record for 15RT280

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: 15RT280   
# Created Wed May  8 01:17:19 2024
# Orbit generated from Bernstein formalism
# Fitting     20 observations of     21
# Arc:   2.35y
# First observation: 2015/07/19
#  Last observation: 2017/11/22
Preliminary a, adot, b, bdot, g, gdot:
  -0.000092   0.021909  -0.000007  -0.004128   0.023639   0.000000
# Chi-squared of fit:     6.88 DOF:     34 RMS:  0.10
# Min/Max residuals:    -0.33    0.26
# Exact a, adot, b, bdot, g, gdot:
  1.462701E-05  2.161808E-02 -3.271715E-06 -4.111768E-03  2.343730E-02  1.256106E-03
# Covariance matrix:
  4.3128E-13  2.0913E-13  1.1060E-14 -9.7093E-14  5.2912E-13  1.3166E-11
  2.0913E-13  5.7093E-13  2.2889E-14 -1.5964E-13  6.3445E-13  2.1410E-11
  1.1060E-14  2.2889E-14  1.4829E-13 -1.2738E-13  3.0538E-14  2.1232E-12
 -9.7093E-14 -1.5964E-13 -1.2738E-13  2.6129E-13 -2.2845E-13 -1.2289E-11
  5.2912E-13  6.3445E-13  3.0538E-14 -2.2845E-13  1.0189E-12  3.0750E-11
  1.3166E-11  2.1410E-11  2.1232E-12 -1.2289E-11  3.0750E-11  1.6298E-09
#      lat0       lon0       xBary       yBary       zBary        JD0
    1.999820    9.192184    0.971043    0.010719   -0.303876  2457223.092249
# Heliocentric elements and errors
Epoch:              2457220.5000  =  2015/07/17
Mean Anomaly:          139.00145 +/-     1.526
Argument of Peri:       26.61856 +/-     1.521
Long of Asc Node:      198.25463 +/-     0.001
Inclination:            10.91315 +/-     0.001
Eccentricity:         0.05353486 +/-    0.0010
Semi-Major Axis:     41.26303826 +/-    0.0059
Time of Perihelion: 2419838.9703 +/-     410.3
Perihelion:          39.05402743 +/-    0.0430
Aphelion:            43.47204910 +/-    0.0431
Period (y)              265.0635 +/-      0.06
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           42.54517166 +/-    0.0018
Ecliptic Y            5.90206215 +/-    0.0003
Ecliptic Z            1.48882939 +/-    0.0001
Ecliptic XDOT        -0.00024435 +/-    0.0000
Ecliptic YDOT         0.00251271 +/-    0.0000
Ecliptic ZDOT        -0.00047485 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   42.97839669 +/-    0.0018
Geocenter to KBO     42.66703792 +/-    0.0018
# Hcoef:  8.67

The following table shows the complete astrometric record for 15RT280. 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 (15RT280) followed by the observatory code and reference code for the source of the astrometry.

2015 07  19.59146  00 30 37.139  +05 28 52.83  25.4r 15RT280   568  C~2nvr      
2015 09  07.56274  00 28 30.049  +05 15 03.47  25.0w 15RT280   568  C~2nvr      
2015 09  09.39169  00 28 22.799  +05 14 14.50  25.1r 15RT280   568  C~2nvr      
2015 09  09.43322  00 28 22.642  +05 14 13.39  25.1r 15RT280   568  C~2nvr      
2015 09  09.47414  00 28 22.471  +05 14 12.22  24.9r 15RT280   568  C~2nvr      
2015 09  10.49775  00 28 18.356  +05 13 44.40  25.5w 15RT280   568  C~2nvr      
2015 09  18.45683  00 27 45.366  +05 09 58.90  25.3w 15RT280   568  C~2nvr      
2015 09  18.49367  00 27 45.204  +05 09 58.20  25.3w 15RT280   568  C~2nvr      
2015 10  08.34456  00 26 19.199  +04 59 57.14  24.9w 15RT280   568  C~2nvr      
2015 10  08.39721  00 26 18.978  +04 59 55.75  25.3w 15RT280   568  C~2nvr      
2015 10  09.31421  00 26 15.026  +04 59 27.45  25.2w 15RT280   568  C~2nvr      
2015 11  10.43997  00 24 12.310  +04 44 13.80  24.7w 15RT280   568  C~2nvr      
2015 12  08.23879  00 23 14.258  +04 35 39.95  24.5w 15RT280   568  C~2nvr      
2016 09  05.48640  00 33 35.417  +05 32 07.00  26.0w 15RT280   568  C~2nvr      
2016 09  06.48188  00 33 31.574  +05 31 41.08  25.4w 15RT280   568  C~2nvr      
2016 09  26.43130  00 32 08.580  +05 22 13.23  25.0w 15RT280   568  C~2nvr      
2016 11  03.31006  00 29 32.589  +05 03 31.27  25.1w 15RT280   568  C~2nvr      
2016 11  03.36248  00 29 32.395  +05 03 30.01  25.5w 15RT280   568  C~2nvr      
2016 12  25.23477  00 28 04.477  +04 49 57.74  25.4w 15RT280   568  C~2nvr      
2017 01  02.28151  00 28 11.020  +04 49 58.47  25.1w 15RT280   568  C~2nvr      
2017 11  22.34219  00 33 34.790  +05 12 33.45  24.6w 15RT280   568  C~2nvr      

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     0.10
     2   0.1368  -2071.32    -0.05     -12.50    -0.02
     3   0.1418  -2190.16    -0.13     -14.67     0.10
     4   0.1419  -2192.75     0.04     -14.76     0.04
     5   0.1420  -2195.56    -0.04     -14.83     0.00
     6   0.1448  -2263.03    -0.01     -16.08     0.04
     7   0.1666  -2804.93     0.00     -28.33    -0.33
     8   0.1667  -2807.43     0.11     -28.01     0.02
     9   0.2211  -4225.81    -0.11     -71.40    -0.04
    10   0.2212  -4229.40     0.13     -71.37     0.11
    11   0.2237  -4294.86     0.08     -73.97     0.02
    12   0.3117  -6342.27    -0.06    -185.74    -0.14
    13   0.3878  -7343.93 (   0.70)   -312.99 (   0.26)
    14   1.1332   2523.24     0.04    -870.07     0.04
    15   1.1359   2460.29    -0.02    -871.33     0.05
    16   1.1905   1097.41     0.01    -905.50     0.03
    17   1.2942  -1486.44     0.05   -1017.54    -0.05
    18   1.2944  -1489.60     0.03   -1017.55     0.10
    19   1.4364  -3017.72     0.26   -1244.65     0.02
    20   1.4584  -2927.59    -0.30   -1282.64    -0.05
    21   2.3457   2052.99    -0.03   -1945.44    -0.04

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.

15RT280    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        41.635    41.658    41.614
ecceobj         0.047     0.050     0.045
incobj         10.859    10.859    10.858
qmin           38.838    38.742    38.871
qmax           44.188    44.425    44.120
amean          41.440    41.463    41.418
amin           41.125    41.143    41.098
amax           41.761    41.787    41.745
emean           0.041     0.044     0.039
emin            0.024     0.026     0.022
emax            0.059     0.063     0.058
imean          12.032    12.028    12.035
imin           10.943    10.941    10.945
imax           12.992    12.989    13.004
excite_mean     0.213     0.213     0.212
fracstop        1.000     1.000     1.000
cjmean          3.018     3.018     3.018

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     179.0     178.8
kozaiamp        180.0     179.9     179.9