Orbit Fit and Astrometric record for 13NM24

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: 13NM24    
# Created Mon Dec  6 02:11:41 2021
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     80 observations of     80
# Arc:  10.13y
# First observation: 2011/07/27
#  Last observation: 2021/09/12
# Chi-squared of fit:    64.91 DOF:    154 RMS:  0.16
# Min/Max residuals:    -0.64    0.43
# Exact a, adot, b, bdot, g, gdot:
  1.226609E-05  1.795257E-02  7.124610E-06  1.017423E-02  2.250311E-02 -3.336531E-03
# Covariance matrix:
  1.1282E-13 -3.8865E-14  2.5868E-14 -1.5838E-14  2.6869E-15 -1.6793E-13
 -3.8865E-14  1.9833E-14 -1.6433E-14  1.0014E-14  6.9892E-15  1.0627E-13
  2.5868E-14 -1.6433E-14  8.9249E-14 -2.4191E-14 -2.9266E-15 -1.0894E-13
 -1.5838E-14  1.0014E-14 -2.4191E-14  9.8530E-15  1.3076E-15  6.6556E-14
  2.6869E-15  6.9892E-15 -2.9266E-15  1.3076E-15  8.8439E-14  1.4808E-14
 -1.6793E-13  1.0627E-13 -1.0894E-13  6.6556E-14  1.4808E-14  7.0595E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
   -9.274572  -39.940558    0.284771   -0.156894   -0.960416  2455769.971146
# Heliocentric elements and errors
Epoch:              2455770.5000  =  2011/07/28
Mean Anomaly:          277.53355 +/-     0.020
Argument of Peri:       83.45604 +/-     0.013
Long of Asc Node:      335.28001 +/-     0.000
Inclination:            30.74104 +/-     0.000
Eccentricity:         0.16541850 +/-    0.0000
Semi-Major Axis:     45.14951348 +/-    0.0023
Time of Perihelion: 2481154.0780 +/-       9.0
Perihelion:          37.68094867 +/-    0.0026
Aphelion:            52.61807828 +/-    0.0032
Period (y)              303.3806 +/-      0.02
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           34.19342074 +/-    0.0004
Ecliptic Y          -28.99829158 +/-    0.0004
Ecliptic Z           -7.16157763 +/-    0.0001
Ecliptic XDOT         0.00124519 +/-    0.0000
Ecliptic YDOT         0.00180936 +/-    0.0000
Ecliptic ZDOT         0.00128715 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   45.40252097 +/-    0.0004
Geocenter to KBO     44.43843534 +/-    0.0006
# Hcoef:  6.21

The following table shows the complete astrometric record for 13NM24. 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 (13NM24) followed by the observatory code and reference code for the source of the astrometry.

2011 07  27.47038  21 42 35.222  -23 34 18.57  22.7w 13NM24    F51  C~1w3u      
2011 07  27.48507  21 42 35.131  -23 34 18.73  23.1w 13NM24    F51  C~1w3u      
2011 07  27.49976  21 42 35.099  -23 34 19.36  22.7w 13NM24    F51  C~1w3u      
2011 07  27.51447  21 42 35.036  -23 34 19.44  22.9w 13NM24    F51  C~1w3u      
2011 08  19.45837  21 40 45.415  -23 41 13.06  21.8i 13NM24    F51  C~1w3u      
2011 08  30.41424  21 39 52.807  -23 43 47.40  22.9w 13NM24    F51  C~1w3u      
2011 08  30.44372  21 39 52.680  -23 43 48.05  23.1w 13NM24    F51  C~1w3u      
2012 08  21.38163  21 43 55.858  -22 48 13.42  22.1w 13NM24    F51  C~1w3u      
2012 08  21.39546  21 43 55.803  -22 48 13.68  22.0w 13NM24    F51  C~1w3u      
2012 08  21.40960  21 43 55.730  -22 48 14.00  22.4w 13NM24    F51  C~1w3u      
2012 11  02.24010  21 40 00.864  -22 49 51.96  22.8G 13NM24    F51  C~2r7P      
2013 07  14.51185  21 50 11.363  -21 41 58.84  22.8w 13NM24    F51  C~1w3u      
2013 07  14.52730  21 50 11.309  -21 41 59.35  22.5w 13NM24    F51  C~1w3u      
2013 07  14.54365  21 50 11.225  -21 41 59.63  22.6w 13NM24    F51  C~1w3u      
2013 08  24.43957  21 47 04.139  -21 54 40.26  23.1G 13NM24    F51  C~2r7P      
2013 08  29.36229  21 46 40.690  -21 55 52.97  22.5w 13NM24    F51  C~1w3u      
2013 08  29.37612  21 46 40.609  -21 55 53.13  22.5w 13NM24    F51  C~1w3u      
2013 08  29.38994  21 46 40.552  -21 55 53.36  22.6w 13NM24    F51  C~1w3u      
2013 08  29.40375  21 46 40.476  -21 55 53.58  22.4w 13NM24    F51  C~1w3u      
2013 08  31.38564  21 46 31.195  -21 56 20.96  22.8G 13NM24    F51  C~2r7P      
2014 06  27.51939  21 54 28.102  -20 41 52.51  22.6G 13NM24    F51  C~2r7P      
2014 06  27.53108  21 54 28.071  -20 41 53.08  22.5G 13NM24    F51  C~2r7P      
2014 06  27.54277  21 54 28.051  -20 41 52.96  22.4G 13NM24    F51  C~2r7P      
2014 06  27.55443  21 54 27.999  -20 41 53.36  23.1G 13NM24    F51  C~2r7P      
2014 07  03.55938  21 54 09.984  -20 43 34.04  22.3G 13NM24    F51  C~2r7P      
2014 07  03.57062  21 54 09.933  -20 43 34.70  23.2G 13NM24    F51  C~2r7P      
2014 07  03.58182  21 54 09.898  -20 43 34.67  22.5G 13NM24    F51  C~2r7P      
2014 07  03.59304  21 54 09.864  -20 43 34.90  23.1G 13NM24    F51  C~2r7P      
2014 07  25.48043  21 52 46.113  -20 50 28.45  22.6G 13NM24    F51  C~2r7P      
2014 07  25.49167  21 52 46.062  -20 50 28.55  23.0G 13NM24    F51  C~2r7P      
2014 07  25.50293  21 52 46.014  -20 50 28.80  22.8G 13NM24    F51  C~2r7P      
2014 07  25.51416  21 52 45.968  -20 50 29.12  22.8G 13NM24    F51  C~2r7P      
2014 08  01.50220  21 52 14.708  -20 52 46.07  22.9G 13NM24    F51  C~2r7P      
2014 08  14.44225  21 51 13.751  -20 56 51.36  22.5G 13NM24    F51  C~2r7P      
2014 08  15.44486  21 51 08.936  -20 57 09.29  22.6G 13NM24    F51  C~2r7P      
2014 08  25.41628  21 50 20.958  -20 59 58.73  22.2G 13NM24    F51  C~2r7P      
2014 08  25.42685  21 50 20.912  -20 59 59.05  22.7G 13NM24    F51  C~2r7Q      
2014 08  25.43742  21 50 20.872  -20 59 59.16  22.9G 13NM24    F51  C~2r7Q      
2014 08  25.44802  21 50 20.815  -20 59 59.43  22.9G 13NM24    F51  C~2r7Q      
2014 09  11.35351  21 49 02.816  -21 03 46.21  23.2G 13NM24    F51  C~2r7Q      
2014 09  29.34575  21 47 51.722  -21 05 54.57  21.8G 13NM24    F51  C~2r7Q      
2015 06  17.57121  21 58 08.585  -19 44 03.96  22.5G 13NM24    F51  C~2r7Q      
2015 06  20.54950  21 58 02.427  -19 44 42.32  22.6G 13NM24    F51  C~2r7Q      
2015 07  18.52240  21 56 34.284  -19 52 30.09  22.8G 13NM24    F51  C~2r7Q      
2015 09  06.36262  21 52 45.388  -20 07 22.41  21.9G 13NM24    F51  C~2r7Q      
2015 09  08.46207  21 52 35.860  -20 07 49.45  22.1G 13NM24    F51  C~2r7Q      
2016 07  05.52288  22 00 35.406  -18 52 37.87  22.9G 13NM24    F51  C~2r7Q      
2016 07  05.54346  22 00 35.330  -18 52 38.39  22.6G 13NM24    F51  C~2r7Q      
2016 07  05.55375  22 00 35.312  -18 52 38.54  21.8G 13NM24    F51  C~2r7Q      
2016 07  08.53159  22 00 25.407  -18 53 29.42  22.6G 13NM24    F51  C~2r7Q      
2016 08  02.46677  21 58 44.499  -19 01 19.75  22.3G 13NM24    F51  C~2r7Q      
2016 08  02.47865  21 58 44.449  -19 01 19.90  23.0G 13NM24    F51  C~2r7Q      
2016 08  02.49053  21 58 44.387  -19 01 20.31  22.6G 13NM24    F51  C~2r7Q      
2016 08  02.50238  21 58 44.350  -19 01 20.44  22.7G 13NM24    F51  C~2r7Q      
2016 08  08.46177  21 58 16.827  -19 03 16.12  22.4G 13NM24    F51  C~2r7Q      
2016 08  08.47245  21 58 16.775  -19 03 16.50  22.7G 13NM24    F51  C~2r7Q      
2016 08  08.48317  21 58 16.732  -19 03 16.56  22.4G 13NM24    F51  C~2r7Q      
2016 08  08.49390  21 58 16.666  -19 03 17.04  22.6G 13NM24    F51  C~2r7Q      
2016 08  11.49832  21 58 02.535  -19 04 14.44  22.6G 13NM24    F51  C~2r7Q      
2016 09  08.41741  21 55 50.989  -19 11 58.62  22.5G 13NM24    F51  C~2r7Q      
2016 09  30.39046  21 54 22.580  -19 15 22.11  22.3G 13NM24    F51  C~2r7Q      
2016 09  30.40205  21 54 22.526  -19 15 22.36  21.8G 13NM24    F51  C~2r7Q      
2017 07  04.55045  22 03 54.876  -17 55 34.39  22.8G 13NM24    F51  C~2r7Q      
2017 07  04.56205  22 03 54.850  -17 55 34.35  22.8G 13NM24    F51  C~2r7Q      
2017 07  04.57368  22 03 54.814  -17 55 34.74  22.3G 13NM24    F51  C~2r7Q      
2017 07  25.48728  22 02 37.609  -18 01 46.07  22.4G 13NM24    F51  C~2r7Q      
2017 08  18.41188  22 00 48.462  -18 09 27.27  22.9G 13NM24    F51  C~2r7Q      
2017 08  30.33120  21 59 51.750  -18 12 56.84  22.5G 13NM24    F51  C~2r7Q      
2017 09  15.32638  21 58 39.464  -18 16 46.10  22.5G 13NM24    F51  C~2r7Q      
2017 09  15.33739  21 58 39.420  -18 16 46.23  22.6G 13NM24    F51  C~2r7Q      
2017 09  15.35940  21 58 39.334  -18 16 46.47  22.7G 13NM24    F51  C~2r7Q      
2017 09  16.37353  21 58 35.023  -18 16 58.34  22.5G 13NM24    F51  C~2r7Q      
2017 09  23.34199  21 58 06.676  -18 18 10.07  22.0G 13NM24    F51  C~2r7Q      
2017 09  23.35297  21 58 06.616  -18 18 10.01  22.8G 13NM24    F51  C~2r7Q      
2017 09  23.36396  21 58 06.585  -18 18 10.27  23.3G 13NM24    F51  C~2r7Q      
2017 09  23.37494  21 58 06.531  -18 18 10.09  22.2G 13NM24    F51  C~2r7Q      
2017 12  12.22452  21 56 58.765  -18 05 53.62  22.8G 13NM24    F51  C~2r7Q      
2021 09  12.144900 22 12 01.068  -14 23 11.08  22.5G 13NM24    G37  C~55NG      
2021 09  12.202800 22 12 00.798  -14 23 12.17        13NM24    G37  C~55NG      
2021 09  12.259630 22 12 00.557  -14 23 12.96        13NM24    G37  C~55NG      

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     0.07       0.00     0.03
     2   0.0000      0.00    -0.27       0.00     0.16
     3   0.0001      0.00     0.27       0.00    -0.18
     4   0.0001      0.00     0.35       0.00     0.02
     5   0.0629      0.00    -0.21       0.00    -0.28
     6   0.0929      0.00    -0.19       0.00     0.17
     7   0.0930      0.00     0.03       0.00    -0.12
     8   1.0703      0.00    -0.17       0.00     0.06
     9   1.0703      0.00     0.03       0.00     0.02
    10   1.0703      0.00    -0.03       0.00    -0.08
    11   1.2697      0.00     0.09       0.00     0.02
    12   1.9659      0.00     0.14       0.00     0.21
    13   1.9659      0.00     0.26       0.00     0.00
    14   1.9660      0.00    -0.02       0.00     0.04
    15   2.0779      0.00     0.11       0.00     0.07
    16   2.0914      0.00    -0.01       0.00     0.14
    17   2.0915      0.00    -0.23       0.00     0.17
    18   2.0915      0.00    -0.09       0.00     0.14
    19   2.0915      0.00    -0.23       0.00     0.11
    20   2.0970      0.00     0.35       0.00     0.03
    21   2.9187      0.00    -0.12       0.00     0.08
    22   2.9187      0.00    -0.08       0.00    -0.30
    23   2.9187      0.00     0.13       0.00     0.01
    24   2.9188      0.00    -0.15       0.00    -0.20
    25   2.9352      0.00     0.22       0.00     0.19
    26   2.9353      0.00     0.01       0.00    -0.28
    27   2.9353      0.00     0.04       0.00    -0.05
    28   2.9353      0.00     0.08       0.00    -0.09
    29   2.9952      0.00     0.07       0.00    -0.16
    30   2.9953      0.00     0.06       0.00    -0.04
    31   2.9953      0.00     0.09       0.00    -0.07
    32   2.9953      0.00     0.14       0.00    -0.16
    33   3.0145      0.00    -0.00       0.00     0.13
    34   3.0499      0.00     0.10       0.00    -0.12
    35   3.0526      0.00     0.14       0.00     0.05
    36   3.0799      0.00    -0.03       0.00     0.08
    37   3.0800      0.00     0.05       0.00    -0.08
    38   3.0800      0.00     0.22       0.00    -0.02
    39   3.0800      0.00     0.14       0.00    -0.12
    40   3.1263      0.00    -0.13       0.00     0.01
    41   3.1756      0.00    -0.24       0.00    -0.10
    42   3.8908      0.00    -0.03       0.00    -0.01
    43   3.8989      0.00    -0.09       0.00     0.10
    44   3.9755      0.00    -0.60       0.00     0.26
    45   4.1120      0.00     0.07       0.00     0.06
    46   4.1177      0.00    -0.17       0.00     0.22
    47   4.9420      0.00    -0.12       0.00     0.14
    48   4.9420      0.00    -0.23       0.00    -0.03
    49   4.9420      0.00     0.01       0.00    -0.01
    50   4.9502      0.00    -0.01       0.00    -0.17
    51   5.0185      0.00    -0.01       0.00    -0.07
    52   5.0185      0.00     0.07       0.00     0.01
    53   5.0185      0.00    -0.04       0.00    -0.17
    54   5.0186      0.00     0.23       0.00    -0.06
    55   5.0349      0.00     0.06       0.00     0.13
    56   5.0349      0.00     0.05       0.00    -0.05
    57   5.0349      0.00     0.17       0.00     0.10
    58   5.0350      0.00    -0.05       0.00    -0.17
    59   5.0432      0.00     0.08       0.00    -0.01
    60   5.1196      0.00    -0.05       0.00     0.08
    61   5.1798      0.00    -0.44       0.00     0.37
    62   5.1798      0.00    -0.64       0.00     0.18
    63   5.9386      0.00    -0.19       0.00    -0.17
    64   5.9386      0.00    -0.03       0.00     0.05
    65   5.9387      0.00    -0.02       0.00    -0.15
    66   5.9959      0.00     0.16       0.00    -0.10
    67   6.0614      0.00     0.43       0.00    -0.02
    68   6.0941      0.00     0.18       0.00     0.23
    69   6.1379      0.00    -0.04       0.00    -0.04
    70   6.1379      0.00     0.02       0.00    -0.04
    71   6.1380      0.00     0.17       0.00    -0.02
    72   6.1407      0.00     0.11       0.00    -0.00
    73   6.1598      0.00     0.22       0.00    -0.06
    74   6.1598      0.00    -0.03       0.00     0.10
    75   6.1599      0.00     0.17       0.00    -0.07
    76   6.1599      0.00     0.01       0.00     0.21
    77   6.3785      0.00    -0.02       0.00    -0.19
    78  10.1292      0.00    -0.01       0.00     0.05
    79  10.1293      0.00    -0.14       0.00    -0.10
    80  10.1295      0.00     0.10       0.00     0.03

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.

13NM24    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        45.073    45.073    45.073
ecceobj         0.166     0.166     0.166
incobj         30.738    30.738    30.738
qmin           36.653    36.748    36.530
qmax           53.864    53.895    54.089
amean          45.086    45.104    45.101
amin           44.701    44.701    44.698
amax           45.532    45.555    45.556
emean           0.159     0.159     0.162
emin            0.137     0.138     0.137
emax            0.185     0.184     0.188
imean          31.837    31.849    31.816
imin           31.337    31.378    31.319
imax           32.210    32.213    32.178
excite_mean     0.551     0.551     0.552
fracstop        1.000     1.000     1.000
cjmean          2.720     2.720     2.720

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     177.5     176.8
kozaiamp        179.9     179.9     179.9