Orbit Fit and Astrometric record for 15KN199

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: 15KN199   
# Created Wed May  8 01:17:13 2024
# Orbit generated from Bernstein formalism
# Fitting     21 observations of     22
# Arc:   1.37y
# First observation: 2015/03/21
#  Last observation: 2016/07/05
Preliminary a, adot, b, bdot, g, gdot:
  -0.000086   0.021562   0.000003  -0.000027   0.022734   0.000000
# Chi-squared of fit:    14.06 DOF:     36 RMS:  0.14
# Min/Max residuals:    -0.53    0.39
# Exact a, adot, b, bdot, g, gdot:
  1.421926E-05  2.118463E-02 -3.061542E-06 -2.680200E-05  2.243363E-02 -6.256808E-04
# Covariance matrix:
  7.9154E-13  1.4155E-13 -5.2679E-14  5.5285E-14  8.3415E-13  4.0110E-11
  1.4155E-13  5.7792E-13 -3.2736E-14  4.8275E-14  5.2089E-13  3.5204E-11
 -5.2679E-14 -3.2736E-14  1.7058E-13 -1.8467E-13 -7.6345E-14 -4.3328E-12
  5.5285E-14  4.8275E-14 -1.8467E-13  3.3476E-13  9.4878E-14  6.8518E-12
  8.3415E-13  5.2089E-13 -7.6345E-14  9.4878E-14  1.2116E-12  6.9026E-11
  4.0110E-11  3.5204E-11 -4.3328E-12  6.8518E-12  6.9026E-11  5.0009E-09
#      lat0       lon0       xBary       yBary       zBary        JD0
    4.851671 -124.593087    0.980443    0.008862   -0.102869  2457074.157438
# Heliocentric elements and errors
Epoch:              2457070.5000  =  2015/02/17
Mean Anomaly:          284.80372 +/-     0.352
Argument of Peri:      170.53034 +/-     0.699
Long of Asc Node:      144.41949 +/-     0.019
Inclination:             4.83906 +/-     0.000
Eccentricity:         0.05001731 +/-    0.0033
Semi-Major Axis:     45.16097205 +/-    0.0148
Time of Perihelion: 2480225.0953 +/-     107.8
Perihelion:          42.90214177 +/-    0.1503
Aphelion:            47.41980234 +/-    0.1505
Period (y)              303.4961 +/-      0.15
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -26.08529848 +/-    0.0013
Ecliptic Y          -36.09178229 +/-    0.0018
Ecliptic Z            3.76995032 +/-    0.0002
Ecliptic XDOT         0.00216774 +/-    0.0000
Ecliptic YDOT        -0.00141104 +/-    0.0000
Ecliptic ZDOT        -0.00000963 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   44.69084997 +/-    0.0016
Geocenter to KBO     44.57592441 +/-    0.0022
# Hcoef:  8.07

The following table shows the complete astrometric record for 15KN199. 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 (15KN199) followed by the observatory code and reference code for the source of the astrometry.

2015 02  20.65666  15 37 03.244  -14 23 58.20  24.2r 15KN199   568  C~4n9t      
2015 03  21.62951  15 36 37.082  -14 19 17.92  24.8r 15KN199   568  C~4n9t      
2015 04  12.48811  15 35 33.322  -14 13 45.73  24.5r 15KN199   568  C~4n9t      
2015 04  12.52910  15 35 33.177  -14 13 44.74  24.4r 15KN199   568  C~4n9t      
2015 05  17.38343  15 33 05.552  -14 03 51.36  24.5r 15KN199   568  C~4n9t      
2015 05  17.42514  15 33 05.365  -14 03 50.83  24.8r 15KN199   568  C~4n9t      
2015 05  24.36910  15 32 33.890  -14 02 01.75  24.2r 15KN199   568  C~4n9t      
2015 05  24.41533  15 32 33.679  -14 02 00.97  23.7r 15KN199   568  C~4n9t      
2015 05  24.45620  15 32 33.487  -14 02 00.31  24.3r 15KN199   568  C~4n9t      
2015 05  26.44379  15 32 24.564  -14 01 30.85  24.5r 15KN199   568  C~4n9t      
2015 06  18.34328  15 30 49.120  -13 56 44.35  24.6r 15KN199   568  C~4n9t      
2015 06  18.38434  15 30 49.005  -13 56 43.75  24.4r 15KN199   568  C~4n9t      
2015 06  21.35896  15 30 38.132  -13 56 15.89  24.6r 15KN199   568  C~4n9t      
2015 07  10.39102  15 29 40.888  -13 54 20.68  24.8r 15KN199   568  C~4n9t      
2015 07  17.34619  15 29 26.180  -13 54 07.72        15KN199   568  C~4n9t      
2015 07  18.31678  15 29 24.395  -13 54 07.00  24.6r 15KN199   568  C~4n9t      
2016 04  08.58811  15 40 42.032  -14 31 55.12  25.1w 15KN199   568  C~4n9t      
2016 04  29.46970  15 39 20.851  -14 26 09.17  24.6w 15KN199   568  C~4n9t      
2016 05  04.40478  15 38 59.311  -14 24 46.05  24.6w 15KN199   568  C~4n9t      
2016 05  30.47820  15 37 01.520  -14 17 59.72  25.2w 15KN199   568  C~4n9t      
2016 07  04.29009  15 34 50.325  -14 12 22.47  25.2w 15KN199   568  C~4n9t      
2016 07  05.35837  15 34 47.316  -14 12 17.43  24.4w 15KN199   568  C~4n9t      

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 (   0.15)      0.00 (   0.63)
     2   0.0793   -435.08    -0.09     183.81     0.03
     3   0.1392  -1413.99     0.07     289.72    -0.18
     4   0.1393  -1416.27     0.09     290.19     0.15
     5   0.2347  -3643.24    -0.10     360.05     0.15
     6   0.2348  -3646.01     0.02     359.92     0.03
     7   0.2538  -4116.98     0.08     357.08     0.06
     8   0.2540  -4120.15     0.07     357.11     0.14
     9   0.2541  -4123.02    -0.01     357.09     0.16
    10   0.2595  -4256.21     0.07     354.81    -0.24
    11   0.3222  -5674.48    -0.53     301.26    -0.35
    12   0.3223  -5676.25     0.01     301.44    -0.01
    13   0.3305  -5836.73    -0.06     290.54     0.06
    14   0.3826  -6674.20     0.05     202.06     0.03
    15   0.4016  -6885.40     0.39     163.03    -0.06
    16   0.4043  -6910.83    -0.04     157.46     0.02
    17   1.1305   3202.19     0.03     270.83    -0.07
    18   1.1877   1975.02    -0.08     336.30    -0.10
    19   1.2012   1651.34     0.05     344.91    -0.01
    20   1.2726   -107.95     0.03     342.76     0.22
    21   1.3679  -2041.29    -0.01     223.66    -0.01
    22   1.3708  -2085.00    -0.04     218.25    -0.02

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.

15KN199    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        44.826    44.862    44.797
ecceobj         0.054     0.062     0.045
incobj          4.842     4.842     4.842
qmin           42.044    41.722    42.396
qmax           48.452    48.921    48.047
amean          45.162    45.195    45.131
amin           44.798    44.830    44.771
amax           45.528    45.581    45.505
emean           0.052     0.061     0.044
emin            0.038     0.047     0.030
emax            0.065     0.074     0.057
imean           4.042     4.047     4.038
imin            3.568     3.566     3.573
imax            4.515     4.529     4.504
excite_mean     0.088     0.093     0.083
fracstop        1.000     1.000     1.000
cjmean          3.106     3.106     3.107

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       182.5     183.5     182.3
kozaiamp        180.0     179.9     180.0