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: 14OJ394 # Created Fri Nov 22 02:09:56 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 71 observations of 71 # Arc: 9.16y # First observation: 2013/07/04 # Last observation: 2022/08/31 # Chi-squared of fit: 32.69 DOF: 136 RMS: 0.12 # Min/Max residuals: -0.25 0.39 # Exact a, adot, b, bdot, g, gdot: 1.293611E-05 1.680067E-02 9.146485E-06 1.135054E-02 2.159158E-02 4.192172E-03 # Covariance matrix: 1.1424E-13 -5.9734E-14 4.5487E-14 -3.5148E-14 9.9075E-15 -3.4820E-13 -5.9734E-14 4.2252E-14 -3.5653E-14 2.7461E-14 -1.7785E-15 2.7196E-13 4.5487E-14 -3.5653E-14 8.4025E-14 -3.6281E-14 6.4079E-16 -2.5297E-13 -3.5148E-14 2.7461E-14 -3.6281E-14 2.3612E-14 -1.6426E-15 1.9491E-13 9.9075E-15 -1.7785E-15 6.4079E-16 -1.6426E-15 7.7361E-14 -1.7393E-14 -3.4820E-13 2.7196E-13 -2.5297E-13 1.9491E-13 -1.7393E-14 1.9303E-12 # lat0 lon0 xBary yBary zBary JD0 -7.897730 -71.896619 0.101548 -0.139336 -1.004488 2456477.934838 # Heliocentric elements and errors Epoch: 2456478.5000 = 2013/07/05 Mean Anomaly: 52.58271 +/- 0.010 Argument of Peri: 270.02266 +/- 0.010 Long of Asc Node: 299.23253 +/- 0.000 Inclination: 34.82158 +/- 0.000 Eccentricity: 0.22372878 +/- 0.0001 Semi-Major Axis: 52.43885201 +/- 0.0046 Time of Perihelion: 2436219.4699 +/- 4.6 Perihelion: 40.70677151 +/- 0.0055 Aphelion: 64.17093251 +/- 0.0070 Period (y) 379.7414 +/- 0.05 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 14.47418107 +/- 0.0002 Ecliptic Y -44.59691361 +/- 0.0006 Ecliptic Z -6.36335670 +/- 0.0001 Ecliptic XDOT 0.00224369 +/- 0.0000 Ecliptic YDOT -0.00002703 +/- 0.0000 Ecliptic ZDOT 0.00135272 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 47.31665199 +/- 0.0005 Geocenter to KBO 46.31422830 +/- 0.0006 # Hcoef: 5.06
The following table shows the complete astrometric record for 14OJ394. 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 (14OJ394) followed by the observatory code and reference code for the source of the astrometry.
2013 07 04.43406 19 23 18.285 -30 02 15.04 21.7w 14OJ394 F51 C~1vXf 2013 07 04.44665 19 23 18.220 -30 02 14.94 21.8w 14OJ394 F51 C~1vXf 2013 07 04.45921 19 23 18.168 -30 02 15.06 21.6w 14OJ394 F51 C~1vXf 2013 07 04.47179 19 23 18.097 -30 02 15.07 21.7w 14OJ394 F51 C~1vXf 2013 07 19.41896 19 22 02.186 -30 02 54.38 21.1G 14OJ394 F51 C~2kQR 2014 06 27.48590 19 27 48.512 -29 14 47.14 22.0G 14OJ394 F51 C~2kQR 2014 07 26.36489 19 25 24.779 -29 16 20.02 21.9w 14OJ394 F51 C~1vXf 2014 07 26.37621 19 25 24.726 -29 16 20.00 21.8w 14OJ394 F51 C~1vXf 2014 07 26.38751 19 25 24.667 -29 16 20.05 21.7w 14OJ394 F51 C~1vXf 2014 07 28.36121 19 25 15.081 -29 16 20.58 21.9w 14OJ394 F51 C~1vXf 2014 07 28.37188 19 25 15.042 -29 16 20.58 22.1w 14OJ394 F51 C~1vXf 2014 07 28.38256 19 25 14.977 -29 16 20.88 21.8w 14OJ394 F51 C~1vXf 2014 08 15.38022 19 23 54.002 -29 15 46.62 21.6G 14OJ394 F51 C~2kQR 2014 08 23.31071 19 23 23.361 -29 15 07.17 22.0w 14OJ394 F51 C~1vXf 2014 08 23.32203 19 23 23.324 -29 15 07.14 21.9w 14OJ394 F51 C~1vXf 2014 08 23.33337 19 23 23.264 -29 15 07.11 22.1w 14OJ394 F51 C~1vXf 2014 08 23.34468 19 23 23.229 -29 15 07.10 22.0w 14OJ394 F51 C~1vXf 2014 09 12.23790 19 22 25.643 -29 12 22.53 21.9w 14OJ394 F51 C~1vXf 2014 09 12.24863 19 22 25.611 -29 12 22.53 22.0w 14OJ394 F51 C~1vXf 2014 09 12.25933 19 22 25.600 -29 12 22.17 21.9w 14OJ394 F51 C~1vXf 2014 09 12.27003 19 22 25.574 -29 12 22.22 21.7w 14OJ394 F51 C~1vXf 2014 09 19.24418 19 22 13.027 -29 11 02.58 22.5G 14OJ394 F51 C~2kQR 2015 05 22.53458 19 34 00.842 -28 23 52.88 22.1w 14OJ394 F51 C~1vXf 2015 05 22.54503 19 34 00.805 -28 23 53.21 22.2w 14OJ394 F51 C~1vXf 2015 05 22.55546 19 34 00.762 -28 23 53.29 22.0w 14OJ394 F51 C~1vXf 2015 05 22.56592 19 34 00.723 -28 23 53.34 22.0w 14OJ394 F51 C~1vXf 2015 05 24.54501 19 33 54.921 -28 24 06.31 21.9w 14OJ394 F51 C~1vXf 2015 05 24.55525 19 33 54.894 -28 24 06.12 21.9w 14OJ394 F51 C~1vXf 2015 05 24.56549 19 33 54.847 -28 24 06.18 21.6w 14OJ394 F51 C~1vXf 2015 05 25.57081 19 33 51.781 -28 24 12.96 22.1w 14OJ394 F51 C~1vXf 2015 05 25.58079 19 33 51.758 -28 24 12.86 22.1w 14OJ394 F51 C~1vXf 2015 05 25.59076 19 33 51.716 -28 24 13.01 22.1w 14OJ394 F51 C~1vXf 2015 05 25.60073 19 33 51.686 -28 24 13.15 21.9w 14OJ394 F51 C~1vXf 2015 06 17.43715 19 32 24.816 -28 26 47.34 21.9w 14OJ394 F51 C~1vXf 2015 06 17.44713 19 32 24.765 -28 26 47.31 21.6w 14OJ394 F51 C~1vXf 2015 06 17.45712 19 32 24.720 -28 26 47.47 21.7w 14OJ394 F51 C~1vXf 2015 06 19.47225 19 32 15.747 -28 27 00.44 21.8w 14OJ394 F51 C~1vXf 2015 06 19.48226 19 32 15.705 -28 27 00.44 22.0w 14OJ394 F51 C~1vXf 2015 06 19.49226 19 32 15.653 -28 27 00.59 21.9w 14OJ394 F51 C~1vXf 2015 06 19.50226 19 32 15.602 -28 27 00.68 21.9w 14OJ394 F51 C~1vXf 2015 07 24.38684 19 29 26.183 -28 29 35.51 21.6i 14OJ394 F51 C~1vXf 2015 07 24.39642 19 29 26.126 -28 29 35.55 21.7i 14OJ394 F51 C~1vXf 2015 07 24.39652 19 29 26.147 -28 29 35.58 22.3G 14OJ394 F51 C~2kQR 2015 07 24.40622 19 29 26.111 -28 29 35.29 23.1G 14OJ394 F51 C~2kQR 2015 07 24.41580 19 29 26.032 -28 29 35.53 21.7i 14OJ394 F51 C~1vXf 2015 07 24.41590 19 29 26.038 -28 29 35.65 22.2G 14OJ394 F51 C~2kQR 2016 07 05.44196 19 34 40.888 -27 41 40.86 21.9G 14OJ394 F51 C~2kQR 2016 07 05.45231 19 34 40.839 -27 41 40.84 21.6G 14OJ394 F51 C~2kQR 2016 07 05.46267 19 34 40.793 -27 41 40.96 21.6G 14OJ394 F51 C~2kQR 2016 07 05.47298 19 34 40.727 -27 41 40.98 21.6G 14OJ394 F51 C~2kQR 2016 08 03.35486 19 32 21.058 -27 43 07.82 22.3G 14OJ394 F51 C~2kQR 2016 08 03.36690 19 32 21.011 -27 43 07.96 22.1G 14OJ394 F51 C~2kQR 2016 08 03.37900 19 32 20.948 -27 43 07.84 21.6G 14OJ394 F51 C~2kQR 2016 08 03.39104 19 32 20.889 -27 43 07.97 22.0G 14OJ394 F51 C~2kQR 2017 05 26.53103 19 41 04.765 -26 50 38.43 22.1G 14OJ394 F51 C~2kQR 2017 05 26.55177 19 41 04.690 -26 50 38.49 21.9G 14OJ394 F51 C~2kQR 2017 06 23.46123 19 39 17.801 -26 53 35.34 22.2G 14OJ394 F51 C~2kQR 2017 07 26.39088 19 36 40.593 -26 56 15.46 21.6G 14OJ394 F51 C~2kQR 2017 08 13.31684 19 35 19.695 -26 56 35.82 21.4G 14OJ394 F51 C~2kQS 2018 05 24.57837 19 44 43.082 -26 03 39.96 21.6G 14OJ394 F51 C~2kQS 2018 05 24.58873 19 44 43.044 -26 03 40.10 22.2G 14OJ394 F51 C~2kQS 2020 06 15.45653 19 50 20.542 -24 32 23.10 21.7w 14OJ394 F51 C~3wpJ 2020 06 15.46666 19 50 20.499 -24 32 22.93 21.8w 14OJ394 F51 C~3wpJ 2020 06 15.47680 19 50 20.447 -24 32 23.20 22.0w 14OJ394 F51 C~3wpJ 2020 06 15.48694 19 50 20.430 -24 32 23.05 22.1w 14OJ394 F51 C~3wpJ 2022 07 04.356070 19 55 42.456 -23 01 17.48 21.9G 14OJ394 G37 C~5i3D 2022 07 04.421260 19 55 42.173 -23 01 18.20 14OJ394 G37 C~5i3D 2022 08 31.295046 19 51 35.020 -23 05 43.27 22.1w 14OJ394 F51 C~5nI7 2022 08 31.303381 19 51 34.994 -23 05 43.08 22.1w 14OJ394 F51 C~5nI7 2022 08 31.311648 19 51 34.953 -23 05 43.05 21.9w 14OJ394 F51 C~5nI7 2022 08 31.319934 19 51 34.934 -23 05 43.14 21.9w 14OJ394 F51 C~5nI7
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 -0.12 0.00 -0.19
2 0.0000 0.00 -0.13 0.00 -0.04
3 0.0001 0.00 0.06 0.00 -0.11
4 0.0001 0.00 -0.03 0.00 -0.07
5 0.0410 0.00 -0.05 0.00 0.28
6 0.9803 0.00 0.16 0.00 -0.11
7 1.0594 0.00 0.08 0.00 -0.08
8 1.0594 0.00 0.13 0.00 -0.06
9 1.0594 0.00 0.08 0.00 -0.10
10 1.0648 0.00 -0.07 0.00 0.05
11 1.0649 0.00 0.14 0.00 0.05
12 1.0649 0.00 -0.05 0.00 -0.25
13 1.1142 0.00 0.00 0.00 -0.15
14 1.1359 0.00 0.02 0.00 0.20
15 1.1359 0.00 0.10 0.00 0.16
16 1.1359 0.00 -0.17 0.00 0.12
17 1.1360 0.00 -0.07 0.00 0.07
18 1.1904 0.00 0.02 0.00 -0.07
19 1.1905 0.00 -0.11 0.00 -0.18
20 1.1905 0.00 0.08 0.00 0.06
21 1.1905 0.00 0.04 0.00 -0.10
22 1.2096 0.00 0.21 0.00 0.05
23 1.8812 0.00 0.23 0.00 0.33
24 1.8812 0.00 0.14 0.00 0.06
25 1.8812 0.00 -0.04 0.00 0.05
26 1.8813 0.00 -0.17 0.00 0.07
27 1.8867 0.00 0.07 0.00 -0.05
28 1.8867 0.00 0.14 0.00 0.21
29 1.8867 0.00 -0.09 0.00 0.22
30 1.8895 0.00 -0.07 0.00 0.04
31 1.8895 0.00 0.06 0.00 0.21
32 1.8895 0.00 -0.09 0.00 0.13
33 1.8896 0.00 -0.07 0.00 0.05
34 1.9521 0.00 0.07 0.00 -0.09
35 1.9521 0.00 -0.02 0.00 0.01
36 1.9522 0.00 -0.02 0.00 -0.09
37 1.9577 0.00 0.07 0.00 -0.06
38 1.9577 0.00 0.13 0.00 0.00
39 1.9577 0.00 0.03 0.00 -0.08
40 1.9578 0.00 -0.04 0.00 -0.11
41 2.0533 0.00 -0.09 0.00 0.04
42 2.0533 0.00 -0.23 0.00 0.02
43 2.0533 0.00 0.09 0.00 -0.01
44 2.0533 0.00 0.28 0.00 0.29
45 2.0533 0.00 -0.19 0.00 0.07
46 2.0533 0.00 -0.10 0.00 -0.05
47 3.0034 0.00 -0.05 0.00 -0.09
48 3.0035 0.00 -0.01 0.00 -0.02
49 3.0035 0.00 0.07 0.00 -0.09
50 3.0035 0.00 -0.16 0.00 -0.06
51 3.0826 0.00 -0.04 0.00 -0.02
52 3.0826 0.00 0.10 0.00 -0.15
53 3.0827 0.00 0.00 0.00 -0.02
54 3.0827 0.00 -0.04 0.00 -0.15
55 3.8935 0.00 -0.00 0.00 -0.05
56 3.8935 0.00 -0.17 0.00 0.01
57 3.9700 0.00 -0.03 0.00 -0.07
58 4.0601 0.00 -0.01 0.00 -0.07
59 4.1092 0.00 0.21 0.00 0.06
60 4.8875 0.00 0.04 0.00 -0.02
61 4.8875 0.00 -0.09 0.00 -0.11
62 6.9487 0.00 0.08 0.00 -0.16
63 6.9488 0.00 0.04 0.00 0.07
64 6.9488 0.00 -0.13 0.00 -0.13
65 6.9488 0.00 0.23 0.00 0.08
66 8.9991 0.00 -0.19 0.00 0.39
67 8.9993 0.00 -0.02 0.00 0.09
68 9.1577 0.00 0.04 0.00 -0.21
69 9.1578 0.00 0.07 0.00 -0.02
70 9.1578 0.00 -0.13 0.00 0.02
71 9.1578 0.00 0.01 0.00 -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.
14OJ394 quality flag:2 Type: SCATEXTD SCATEXTD SCATNEAR axisobj 52.374 52.374 52.373 ecceobj 0.221 0.221 0.221 incobj 34.764 34.764 34.764 qmin 40.227 40.241 40.259 qmax 65.676 65.656 65.717 amean 52.685 52.685 52.685 amin 52.213 52.196 52.203 amax 53.254 53.246 53.263 emean 0.217 0.217 0.217 emin 0.202 0.202 0.202 emax 0.234 0.234 0.234 imean 36.451 36.452 36.451 imin 36.169 36.169 36.168 imax 36.773 36.766 36.775 excite_mean 0.632 0.632 0.632 fracstop 1.000 1.000 1.000 cjmean 2.647 2.647 2.647 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 175.3 175.3 175.3 kozaiamp 180.0 180.0 180.0