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: 00YE2 # Created Fri Apr 19 01:10:23 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 16 observations of 16 # Arc: 20.07y # First observation: 2000/12/17 # Last observation: 2021/01/11 # Chi-squared of fit: 30.34 DOF: 26 RMS: 0.24 # Min/Max residuals: -0.55 0.40 # Exact a, adot, b, bdot, g, gdot: 1.703347E-05 2.705947E-02 -2.745560E-06 -1.777155E-03 2.552078E-02 -3.688066E-03 # Covariance matrix: 3.6950E-13 -3.8524E-13 -2.1028E-14 2.6298E-14 1.0376E-12 -6.2207E-13 -3.8524E-13 9.3798E-12 5.3099E-13 -6.9418E-13 -5.2694E-11 1.6928E-11 -2.1028E-14 5.3099E-13 2.3446E-13 -5.0742E-14 -2.9846E-12 9.5855E-13 2.6298E-14 -6.9418E-13 -5.0742E-14 5.3326E-14 3.9103E-12 -1.2535E-12 1.0376E-12 -5.2694E-11 -2.9846E-12 3.9103E-12 3.0360E-10 -9.5491E-11 -6.2207E-13 1.6928E-11 9.5855E-13 -1.2535E-12 -9.5491E-11 3.0576E-11 # lat0 lon0 xBary yBary zBary JD0 -0.831342 56.222713 -0.482335 -0.012525 -0.851654 2451895.643783 # Heliocentric elements and errors Epoch: 2451896.5000 = 2000/12/18 Mean Anomaly: 332.07932 +/- 46.063 Argument of Peri: 234.85581 +/- 0.010 Long of Asc Node: 224.60778 +/- 0.001 Inclination: 3.81249 +/- 0.000 Eccentricity: 0.21163606 +/- 0.4281 Semi-Major Axis: 48.46147645 +/- 0.0100 Time of Perihelion: 2461453.3962 +/- 15767.0 Perihelion: 38.20528060 +/- 20.7480 Aphelion: 58.71767229 +/- 20.7480 Period (y) 337.3674 +/- 0.10 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 21.85937239 +/- 0.1715 Ecliptic Y 33.54767536 +/- 0.2564 Ecliptic Z -0.56862124 +/- 0.0044 Ecliptic XDOT -0.00264244 +/- 0.0000 Ecliptic YDOT 0.00128694 +/- 0.0000 Ecliptic ZDOT -0.00018471 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 40.04508144 +/- 0.2332 Geocenter to KBO 39.18389171 +/- 0.3085 # Hcoef: 8.26
The following table shows the complete astrometric record for 00YE2. 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 (00YE2) followed by the observatory code and reference code for the source of the astrometry.
2000 12 17.14304 03 36 26.98 +18 29 56.3 23.5R 00YE2 695 Cc4111 2000 12 17.18970 03 36 26.80 +18 29 55.5 23.9R 00YE2 695 Cc4111 2000 12 17.23702 03 36 26.53 +18 29 54.4 23.8R 00YE2 695 Cc4111 2000 12 18.11934 03 36 22.70 +18 29 41.0 00YE2 695 Cc4111 2002 11 29.28335 03 51 03.68 +19 04 58.3 00YE2 568 Ck2971 2002 11 30.25206 03 50 58.59 +19 04 42.0 23.9R 00YE2 568 Ck2971 2002 11 30.28801 03 50 58.41 +19 04 41.3 24.2R 00YE2 568 Ck2971 2002 11 30.32542 03 50 58.21 +19 04 40.8 24.2R 00YE2 568 Ck2971 2003 10 28.19232 04 00 28.28 +19 27 24.7 00YE2 309 Ck2971 2003 10 28.24405 04 00 28.04 +19 27 23.6 00YE2 309 Ck2971 2003 10 29.23996 04 00 23.48 +19 27 08.9 00YE2 309 Ck2971 2014 10 22.39487 05 17 06.59 +20 52 49.5 23.9R 00YE2 G37 C~1BxA 2014 10 22.48692 05 17 06.31 +20 52 48.9 00YE2 G37 C~1BxA 2021 01 11.302370 05 53 45.286 +20 41 00.21 23.8G 00YE2 G37 C~4Tvq 2021 01 11.347580 05 53 45.071 +20 41 00.80 00YE2 G37 C~4Tvq 2021 01 11.392640 05 53 44.804 +20 41 00.13 00YE2 G37 C~4Tvq
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 -0.14 0.00 0.32
2 0.0001 0.00 0.31 0.00 0.23
3 0.0003 0.00 -0.55 0.00 -0.14
4 0.0027 0.00 -0.05 0.00 -0.01
5 1.9497 0.00 0.27 0.00 -0.31
6 1.9524 0.00 0.04 0.00 -0.21
7 1.9525 0.00 0.20 0.00 -0.31
8 1.9526 0.00 0.18 0.00 -0.19
9 2.8612 0.00 -0.29 0.00 0.32
10 2.8613 0.00 -0.26 0.00 -0.02
11 2.8641 0.00 0.31 0.00 0.27
12 13.8460 0.00 -0.15 0.00 0.04
13 13.8463 0.00 0.01 0.00 0.07
14 20.0689 0.00 -0.04 0.00 -0.19
15 20.0690 0.00 0.30 0.00 0.40
16 20.0691 0.00 -0.17 0.00 -0.26
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.
00YE2 quality flag:3 Type: 2:1E 2:1E 2:1E axisobj 48.418 48.418 48.418 ecceobj 0.210 0.210 0.210 incobj 3.813 3.813 3.813 qmin 37.627 37.640 37.616 qmax 58.822 58.780 58.873 amean 47.797 47.797 47.797 amin 47.184 47.176 47.194 amax 48.468 48.494 48.470 emean 0.194 0.195 0.194 emin 0.177 0.176 0.177 emax 0.215 0.214 0.215 imean 5.109 5.104 5.120 imin 4.480 4.478 4.462 imax 5.542 5.541 5.543 excite_mean 0.214 0.214 0.214 fracstop 1.000 1.000 1.000 cjmean 3.091 3.091 3.091 libcent 0 180.8 179.6 180.1 libamp 0 148.0 147.5 147.3 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 180.2 180.5 179.2 kozaiamp 179.9 179.9 179.8