Orbit Fit and Astrometric record for 15RV280

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: 15RV280   
# Created Tue Apr  1 01:10:34 2025
# Orbit generated from Bernstein formalism
# Fitting     22 observations of     22
# Arc:   1.55y
# First observation: 2015/07/14
#  Last observation: 2017/01/29
Preliminary a, adot, b, bdot, g, gdot:
  -0.000038   0.028896   0.000014   0.005292   0.027104   0.000000
# Chi-squared of fit:    16.55 DOF:     38 RMS:  0.15
# Min/Max residuals:    -0.49    0.39
# Exact a, adot, b, bdot, g, gdot:
  1.791525E-05  2.831591E-02  1.816452E-06  5.259441E-03  2.664610E-02  9.972170E-04
# Covariance matrix:
  3.6086E-13  3.8597E-13 -3.1255E-14  1.7655E-13  6.3578E-13  2.2179E-11
  3.8597E-13  1.3190E-12 -7.3427E-14  4.3249E-13  1.3901E-12  5.4402E-11
 -3.1255E-14 -7.3427E-14  1.3323E-13 -1.4657E-13 -8.9387E-14 -4.0879E-12
  1.7655E-13  4.3249E-13 -1.4657E-13  4.1451E-13  5.1631E-13  2.6216E-11
  6.3578E-13  1.3901E-12 -8.9387E-14  5.1631E-13  1.7517E-12  6.4907E-11
  2.2179E-11  5.4402E-11 -4.0879E-12  2.6216E-11  6.4907E-11  3.3057E-09
#      lat0       lon0       xBary       yBary       zBary        JD0
    1.695285    9.245819    0.993415    0.006619   -0.220320  2457218.034449
# Heliocentric elements and errors
Epoch:              2457210.5000  =  2015/07/07
Mean Anomaly:            3.36354 +/-     0.873
Argument of Peri:        4.80395 +/-     1.107
Long of Asc Node:      358.79605 +/-     0.001
Inclination:            10.71673 +/-     0.001
Eccentricity:         0.11458115 +/-    0.0002
Semi-Major Axis:     42.63287135 +/-    0.0046
Time of Perihelion: 2456260.5320 +/-     246.6
Perihelion:          37.74794811 +/-    0.0105
Aphelion:            47.51779460 +/-    0.0110
Period (y)              278.3717 +/-      0.05
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           37.39875112 +/-    0.0018
Ecliptic Y            5.08244157 +/-    0.0003
Ecliptic Z            1.11037835 +/-    0.0001
Ecliptic XDOT        -0.00038443 +/-    0.0000
Ecliptic YDOT         0.00287922 +/-    0.0000
Ecliptic ZDOT         0.00054326 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   37.75884980 +/-    0.0018
Geocenter to KBO     37.52893840 +/-    0.0019
# Hcoef:  9.38

The following table shows the complete astrometric record for 15RV280. 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 (15RV280) followed by the observatory code and reference code for the source of the astrometry.

2015 07  14.53366  00 31 17.963  +05 13 21.46  25.1r 15RV280   568  C~2nvr      
2015 07  19.49853  00 31 14.823  +05 13 31.38  25.2r 15RV280   568  C~2nvr      
2015 08  11.49021  00 30 31.271  +05 11 08.92  25.5r 15RV280   568  C~2nvr      
2015 08  11.55462  00 30 31.070  +05 11 07.92  25.0r 15RV280   568  C~2nvr      
2015 08  19.58390  00 30 05.698  +05 09 09.11  25.8r 15RV280   568  C~2nvr      
2015 09  07.56274  00 28 49.346  +05 02 34.81  25.4w 15RV280   568  C~2nvr      
2015 09  09.39169  00 28 41.056  +05 01 49.59  25.1r 15RV280   568  C~2nvr      
2015 09  09.43322  00 28 40.866  +05 01 48.62  25.2r 15RV280   568  C~2nvr      
2015 09  09.47414  00 28 40.669  +05 01 47.69  24.9r 15RV280   568  C~2nvr      
2015 09  10.46103  00 28 36.133  +05 01 22.95  24.8w 15RV280   568  C~2nvr      
2015 09  18.49367  00 27 57.965  +04 57 51.82  25.2w 15RV280   568  C~2nvr      
2015 10  03.37463  00 26 44.153  +04 50 50.52  24.9w 15RV280   568  C~2nvr      
2015 10  08.34456  00 26 19.392  +04 48 26.35  25.2w 15RV280   568  C~2nvr      
2015 10  08.39721  00 26 19.145  +04 48 24.75  25.3w 15RV280   568  C~2nvr      
2016 09  05.48640  00 34 31.487  +05 59 00.24        15RV280   568  C~2nvr      
2016 09  06.44060  00 34 27.285  +05 58 37.95        15RV280   568  C~2nvr      
2016 09  26.43130  00 32 51.939  +05 49 54.19  25.4w 15RV280   568  C~2nvr      
2016 09  26.44752  00 32 51.865  +05 49 54.08  25.3w 15RV280   568  C~2nvr      
2016 11  03.39147  00 29 52.410  +05 32 15.20        15RV280   568  C~2nvr      
2016 11  03.45641  00 29 52.145  +05 32 13.35        15RV280   568  C~2nvr      
2016 12  25.23477  00 28 10.914  +05 21 25.07  25.8w 15RV280   568  C~2nvr      
2017 01  29.24980  00 29 29.100  +05 29 30.08  25.2w 15RV280   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    -0.23       0.00     0.27
     2   0.0136    -39.19    -0.02      27.61    -0.14
     3   0.0765   -693.23     0.13     153.29     0.16
     4   0.0767   -696.39    -0.10     153.55     0.05
     5   0.0987  -1091.55     0.39     193.95    -0.49
     6   0.1507  -2295.38    -0.09     282.20     0.11
     7   0.1557  -2427.05    -0.07     289.61    -0.06
     8   0.1558  -2430.05     0.00     289.84    -0.03
     9   0.1559  -2433.12    -0.04     290.15     0.09
    10   0.1586  -2505.17     0.04     294.21     0.08
    11   0.1806  -3112.63     0.05     325.76     0.13
    12   0.2213  -4292.82     0.08     375.31    -0.06
    13   0.2349  -4689.94    -0.16     389.46    -0.00
    14   0.2351  -4693.97     0.07     389.45    -0.18
    15   1.1470   3734.27     0.08    1380.67     0.11
    16   1.1496   3667.84     0.14    1384.80    -0.01
    17   1.2044   2153.55    -0.23    1462.74    -0.12
    18   1.2044   2152.50     0.02    1463.08     0.15
    19   1.3083   -726.76    -0.14    1545.86     0.19
    20   1.3085   -731.12    -0.21    1545.72    -0.04
    21   1.4502  -2376.02     0.12    1547.46    -0.14
    22   1.5461  -1111.72     0.19    1531.59    -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.

15RV280    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        43.080    43.112    43.050
ecceobj         0.124     0.125     0.123
incobj         10.669    10.670    10.669
qmin           36.724    36.693    36.766
qmax           49.212    49.345    49.177
amean          42.831    42.861    42.802
amin           42.478    42.506    42.451
amax           43.213    43.248    43.184
emean           0.118     0.120     0.117
emin            0.099     0.102     0.099
emax            0.140     0.141     0.139
imean          10.275    10.265    10.258
imin            9.278     9.270     9.224
imax           11.481    11.482    11.479
excite_mean     0.214     0.215     0.213
fracstop        1.000     1.000     1.000
cjmean          3.033     3.033     3.033

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       176.0     175.9     177.0
kozaiamp        180.0     180.0     179.9