La comète Elenin au plus proche de la Terre le 16 et 17 octobre : accrochez vos ceintures !
Publié par Brujitafr
sur
15 Octobre 2011, 06:23am
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#AIR DU TEMPS
Forts séismes et éruptions volcaniques dans les prochains jours ?
Ci-dessous, pour vous confirmer que la comète (?) n'a pas été désintégrée, le rapport de la Nasa
http://ssd.jpl.nasa.gov/sbdb.cgi?sstr=elenin;orb=1;cov=1;log=0;cad=1#cad
[ hide orbit diagram ]
Orbit Diagram | Note: Make sure you have Java enabled on your browser to see the applet. This applet is provided as a 3D orbit visualization tool. The applet was implemented using 2-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances. For accurate long-term ephemerides, please instead use our Horizons system. | | Additional Notes: the orbits shown in the applet are color coded. The planets are white lines, and the asteroid/comet is a blue line. The bright white line indicates the portion of the orbit that is above the ecliptic plane, and the darker portion is below the ecliptic plane. Likewise for the asteroid/comet orbit, the light blue indicates the portion above the ecliptic plane, and the dark blue the portion below the ecliptic plane. Orbit Viewer applet originally written and kindly provided byOsamu Ajiki(AstroArts), and further modified byRon Baalke(JPL). | | |
Orbital Elements at Epoch 2455650.5 (2011-Mar-30.0) TDB Reference: JPL 36 (heliocentric ecliptic J2000) Element | Value | Uncertainty (1-sigma) | Units | e | 1.000064048145741 | 1.8591e-06 | | a | -7532.31733028152 | 218.63 | AU | q | .4824309581374332 | 2.4495e-06 | AU | i | 1.839475154920383 | 4.7959e-05 | deg | node | 323.2338494998166 | 0.00094556 | deg | peri | 343.798953487708 | 0.00093397 | deg | M | 359.999751654787 | 1.0812e-05 | deg | tp | 2455815.219354417315 (2011-Sep-10.71935442) | 0.00037603 | JED | period | n/a n/a | n/a n/a | d yr | n | 1.507686900885618E-6 | 6.5641e-08 | deg/d | Q | n/a | n/a | AU | | | Orbit Determination Parameters Additional Information |
[ hide covariance matrix ]
Orbit Covariance (6×6) | e | q | tp | node | peri | i | e | 3.456207263765826E-12 | 1.200984161232074E-12 | -5.192195588897656E-10 | -1.188784682159179E-10 | -1.54407534555451E-10 | -6.279889138301894E-12 | q | 1.200984161232074E-12 | 6.000089059503247E-12 | -6.668591282280052E-10 | -4.086490262574901E-10 | -4.543306299187816E-11 | -2.516011401592897E-11 | tp | -5.192195588897656E-10 | -6.668591282280052E-10 | 1.414008650272228E-7 | 4.700030314080427E-8 | 2.697170502885165E-8 | 2.922576770841947E-9 | node | -1.188784682159179E-10 | -4.086490262574901E-10 | 4.700030314080427E-8 | 8.940795864805675E-7 | -8.607598023180779E-7 | 4.466869390853531E-8 | peri | -1.54407534555451E-10 | -4.543306299187816E-11 | 2.697170502885165E-8 | -8.607598023180779E-7 | 8.72298754793263E-7 | -4.267381663020393E-8 | i | -6.279889138301894E-12 | -2.516011401592897E-11 | 2.922576770841947E-9 | 4.466869390853531E-8 | -4.267381663020393E-8 | 2.30009065073777E-9 | |
[ hide close-approach data ]
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