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: 99JE132 # Created Sat Apr 27 01:09:52 2024 # Orbit generated from Bernstein formalism # Fitting 55 observations of 55 # Arc: 9.08d # First observation: 1999/05/10 # Last observation: 1999/05/19 Preliminary a, adot, b, bdot, g, gdot: 0.000001 0.027142 -0.000000 0.011644 0.027351 0.000000 # WARNING MRQMIN stopped after 13 iterations -- oscilliatory solution # WARNING Fitting with energy constraint # WARNING MRQMIN stopped after 13 iterations -- oscilliatory solution # WARNING MRQMIN stopped after 13 iterations -- oscilliatory solution # Chi-squared of fit: 27.88 DOF: 105 RMS: 0.13 # Min/Max residuals: -0.32 0.27 # Exact a, adot, b, bdot, g, gdot: 1.372188E-05 2.169942E-02 6.799159E-06 1.166354E-02 2.644274E-02 -1.172060E-02 # Covariance matrix: 7.1181E-12 1.1143E-08 3.6685E-16 -1.2541E-11 1.9136E-09 -1.4755E-09 1.1143E-08 1.7619E-05 7.9677E-13 -2.0170E-08 3.0244E-06 -3.5562E-06 3.6685E-16 7.9677E-13 6.4491E-14 -2.8880E-12 1.1714E-13 -3.6019E-11 -1.2541E-11 -2.0170E-08 -2.8880E-12 2.5851E-10 -3.4310E-09 6.1179E-08 1.9136E-09 3.0244E-06 1.1714E-13 -3.4310E-09 5.1921E-07 -4.9964E-07 -1.4755E-09 -3.5562E-06 -3.6019E-11 6.1179E-08 -4.9964E-07 2.0317E-04 # lat0 lon0 xBary yBary zBary JD0 -0.183516 -147.636687 -0.287291 -0.003331 -0.974171 2451308.685963 # Heliocentric elements and errors Epoch: 2451300.5000 = 1999/05/02 Mean Anomaly: 299.88327 +/- 60.642 Argument of Peri: 109.76158 +/- 35.364 Long of Asc Node: 213.12603 +/- 0.076 Inclination: 28.25940 +/- 4.639 Eccentricity: 0.42700372 +/- 0.4619 Semi-Major Axis: 40.46077540 +/- 21.1609 Time of Perihelion: 2466998.4379 +/- 9954.4 Perihelion: 23.18387371 +/- 22.2775 Aphelion: 57.73767708 +/- 35.5120 Period (y) 257.3709 +/- 201.91 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -32.60393106 +/- 0.8705 Ecliptic Y -21.00682254 +/- 0.5516 Ecliptic Z -0.12088047 +/- 0.0033 Ecliptic XDOT 0.00222173 +/- 0.0013 Ecliptic YDOT -0.00124154 +/- 0.0008 Ecliptic ZDOT 0.00121154 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 38.78553243 +/- 0.7904 Geocenter to KBO 37.81756032 +/- 1.0305 # Hcoef: 8.54
The following table shows the complete astrometric record for 99JE132. 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 (99JE132) followed by the observatory code and reference code for the source of the astrometry.
1999 05 10.18522 14 00 26.47 -12 27 58.0 24.2R 99JE132 807 Ca5620 1999 05 10.19209 14 00 26.45 -12 27 57.7 24.2R 99JE132 807 Ca5620 1999 05 10.19896 14 00 26.41 -12 27 57.6 24.2R 99JE132 807 Ca5620 1999 05 10.20584 14 00 26.38 -12 27 57.4 23.9R 99JE132 807 Ca5620 1999 05 10.21271 14 00 26.34 -12 27 57.1 23.8R 99JE132 807 Ca5620 1999 05 10.21958 14 00 26.30 -12 27 57.1 23.5R 99JE132 807 Ca5620 1999 05 10.22645 14 00 26.29 -12 27 56.7 24.4R 99JE132 807 Ca5620 1999 05 10.23333 14 00 26.24 -12 27 56.6 24.0R 99JE132 807 Ca5620 1999 05 10.24021 14 00 26.21 -12 27 56.0 23.9R 99JE132 807 Ca5620 1999 05 10.24708 14 00 26.19 -12 27 56.1 24.4R 99JE132 807 Ca5620 1999 05 10.25395 14 00 26.14 -12 27 55.9 23.7R 99JE132 807 Ca5620 1999 05 10.26082 14 00 26.13 -12 27 55.6 24.0R 99JE132 807 Ca5620 1999 05 10.26769 14 00 26.08 -12 27 55.3 23.4R 99JE132 807 Ca5620 1999 05 10.27456 14 00 26.02 -12 27 55.2 23.3R 99JE132 807 Ca5620 1999 05 11.17804 14 00 21.73 -12 27 25.5 24.5R 99JE132 807 Ca5620 1999 05 11.21239 14 00 21.57 -12 27 24.6 24.4R 99JE132 807 Ca5620 1999 05 11.21926 14 00 21.54 -12 27 24.4 24.1R 99JE132 807 Ca5620 1999 05 11.22613 14 00 21.51 -12 27 24.0 24.1R 99JE132 807 Ca5620 1999 05 11.23987 14 00 21.44 -12 27 23.6 24.3R 99JE132 807 Ca5620 1999 05 11.24674 14 00 21.41 -12 27 23.4 24.2R 99JE132 807 Ca5620 1999 05 11.25362 14 00 21.38 -12 27 23.1 24.1R 99JE132 807 Ca5620 1999 05 11.26048 14 00 21.34 -12 27 22.8 24.6R 99JE132 807 Ca5620 1999 05 11.26735 14 00 21.32 -12 27 22.9 23.9R 99JE132 807 Ca5620 1999 05 11.27422 14 00 21.28 -12 27 22.4 24.2R 99JE132 807 Ca5620 1999 05 18.17305 13 59 49.31 -12 23 41.7 24.2R 99JE132 807 Ca5620 1999 05 18.18001 13 59 49.30 -12 23 41.2 23.8R 99JE132 807 Ca5620 1999 05 18.18765 13 59 49.28 -12 23 41.3 24.1R 99JE132 807 Ca5620 1999 05 18.19452 13 59 49.23 -12 23 40.8 23.8R 99JE132 807 Ca5620 1999 05 18.20139 13 59 49.20 -12 23 40.8 24.0R 99JE132 807 Ca5620 1999 05 18.20826 13 59 49.18 -12 23 40.5 24.1R 99JE132 807 Ca5620 1999 05 18.21515 13 59 49.16 -12 23 40.3 24.4R 99JE132 807 Ca5620 1999 05 18.22202 13 59 49.09 -12 23 40.2 24.0R 99JE132 807 Ca5620 1999 05 18.22889 13 59 49.08 -12 23 39.8 24.5R 99JE132 807 Ca5620 1999 05 18.23605 13 59 49.03 -12 23 39.7 24.3R 99JE132 807 Ca5620 1999 05 18.24293 13 59 49.00 -12 23 39.3 24.1R 99JE132 807 Ca5620 1999 05 18.24980 13 59 48.98 -12 23 39.4 24.3R 99JE132 807 Ca5620 1999 05 18.25677 13 59 48.95 -12 23 38.9 24.2R 99JE132 807 Ca5620 1999 05 18.26364 13 59 48.92 -12 23 38.9 24.3R 99JE132 807 Ca5620 1999 05 18.27050 13 59 48.90 -12 23 38.8 24.0R 99JE132 807 Ca5620 1999 05 19.12854 13 59 45.06 -12 23 11.8 24.5R 99JE132 807 Ca5620 1999 05 19.13541 13 59 45.04 -12 23 11.6 24.0R 99JE132 807 Ca5620 1999 05 19.14229 13 59 45.00 -12 23 11.5 24.1R 99JE132 807 Ca5620 1999 05 19.14915 13 59 44.97 -12 23 11.3 24.3R 99JE132 807 Ca5620 1999 05 19.15607 13 59 44.94 -12 23 11.0 24.2R 99JE132 807 Ca5620 1999 05 19.16294 13 59 44.91 -12 23 10.6 24.0R 99JE132 807 Ca5620 1999 05 19.16982 13 59 44.87 -12 23 10.4 24.0R 99JE132 807 Ca5620 1999 05 19.17669 13 59 44.85 -12 23 10.4 23.9R 99JE132 807 Ca5620 1999 05 19.18356 13 59 44.81 -12 23 10.2 24.3R 99JE132 807 Ca5620 1999 05 19.19043 13 59 44.79 -12 23 10.0 24.4R 99JE132 807 Ca5620 1999 05 19.19730 13 59 44.74 -12 23 09.7 23.9R 99JE132 807 Ca5620 1999 05 19.23442 13 59 44.60 -12 23 08.4 23.8R 99JE132 807 Ca5620 1999 05 19.24130 13 59 44.56 -12 23 08.6 24.0R 99JE132 807 Ca5620 1999 05 19.24817 13 59 44.53 -12 23 08.2 23.8R 99JE132 807 Ca5620 1999 05 19.25504 13 59 44.49 -12 23 07.9 23.9R 99JE132 807 Ca5620 1999 05 19.26191 13 59 44.47 -12 23 07.8 23.9R 99JE132 807 Ca5620
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 0.04
2 0.0000 -0.38 0.01 0.18 0.17
3 0.0000 -0.96 -0.04 0.07 0.02
4 0.0001 -1.44 0.02 0.11 0.02
5 0.0001 -2.10 -0.10 0.19 0.05
6 0.0001 -2.65 -0.11 -0.01 -0.19
7 0.0001 -2.92 0.15 0.31 0.09
8 0.0001 -3.64 -0.03 0.16 -0.11
9 0.0002 -4.26 -0.11 0.57 0.25
10 0.0002 -4.50 0.18 0.37 0.01
11 0.0002 -5.26 -0.04 0.31 -0.09
12 0.0002 -5.50 0.26 0.54 0.09
13 0.0002 -6.29 0.00 0.57 0.08
14 0.0002 -7.15 -0.32 0.36 -0.18
15 0.0027 -76.37 -0.16 6.62 0.04
16 0.0028 -78.88 0.01 6.66 -0.14
17 0.0028 -79.36 0.06 6.70 -0.15
18 0.0028 -79.91 0.04 6.92 0.03
19 0.0029 -81.01 0.01 6.95 -0.03
20 0.0029 -81.49 0.06 6.98 -0.04
21 0.0029 -82.01 0.08 7.11 0.04
22 0.0029 -82.66 -0.04 7.19 0.08
23 0.0030 -82.90 0.25 7.00 -0.16
24 0.0030 -83.62 0.06 7.27 0.06
25 0.0219 -599.30 -0.29 53.17 -0.16
26 0.0219 -599.61 -0.09 53.59 0.22
27 0.0219 -599.85 0.24 53.39 -0.03
28 0.0219 -600.71 -0.12 53.61 0.15
29 0.0219 -601.13 -0.02 53.46 -0.05
30 0.0220 -601.50 0.10 53.64 0.09
31 0.0220 -601.85 0.27 53.72 0.13
32 0.0220 -602.85 -0.22 53.46 -0.17
33 0.0220 -603.12 0.01 53.79 0.11
34 0.0220 -603.84 -0.19 53.63 -0.10
35 0.0221 -604.39 -0.24 53.85 0.08
36 0.0221 -604.63 0.03 53.66 -0.16
37 0.0221 -605.22 -0.05 53.98 0.11
38 0.0221 -605.63 0.05 53.83 -0.08
39 0.0221 -605.94 0.24 53.82 -0.14
40 0.0245 -668.06 -0.08 59.77 0.03
41 0.0245 -668.40 0.07 59.86 0.08
42 0.0245 -668.99 -0.01 59.75 -0.07
43 0.0245 -669.47 0.01 59.79 -0.08
44 0.0246 -669.98 0.00 59.92 0.01
45 0.0246 -670.54 -0.05 60.14 0.19
46 0.0246 -671.15 -0.16 60.13 0.13
47 0.0246 -671.43 0.06 60.03 -0.02
48 0.0246 -672.05 -0.05 60.01 -0.07
49 0.0247 -672.39 0.10 60.10 -0.03
50 0.0247 -673.18 -0.19 60.13 -0.05
51 0.0248 -675.56 0.14 60.64 0.23
52 0.0248 -676.04 0.16 60.25 -0.21
53 0.0248 -676.59 0.11 60.48 -0.03
54 0.0248 -677.24 -0.04 60.56 0.01
55 0.0249 -677.55 0.15 60.55 -0.05
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.
99JE132 quality flag:0 Type: ERR2LARGE ERR2LARGE ERR2LARGE axisobj 0.000 0.000 0.000 ecceobj -1.000 -1.000 -1.000 incobj -1.000 -1.000 -1.000 qmin 0.000 0.000 0.000 qmax 0.000 0.000 0.000 amean 0.000 0.000 0.000 amin 0.000 0.000 0.000 amax 0.000 0.000 0.000 emean 0.000 0.000 0.000 emin 0.000 0.000 0.000 emax 0.000 0.000 0.000 imean 0.000 0.000 0.000 imin 0.000 0.000 0.000 imax 0.000 0.000 0.000 excite_mean 0.000 0.000 0.000 fracstop 0.000 0.000 0.000 cjmean 0.000 0.000 0.000 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 0.0 0.0 0.0 kozaiamp 0.0 0.0 0.0