File:Schematic-of-maneuvers-and-encounters-leading-to-the-final-TESS-orbit-fr.png

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Français : Schéma des manœuvres effectuées par le télescope spatial TESS pour se placer sur sont orbite finale. 1 -Le télescope est placé sur une orbite haute et élève en deux orbite son apogée en utilisant sa propulsion 2 -- L'assistance gravitationnelle de la Lune qu'il survole est utilisée pour modifier son inclinaison orbitale qui atteint au final 40° par rapport au plan de l'écliptique. 3 - Des corrections avec sa propulsion permettent d'atteindre l'orbite finale avec un apogée et un périgée respectivement à 120 000 km et 400 000 km de la Terre.
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Source https://heasarc.gsfc.nasa.gov/docs/tess/operations.html
Author NASA

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Public domain This file is in the public domain in the United States because it was solely created by NASA. NASA copyright policy states that "NASA material is not protected by copyright unless noted". (See Template:PD-USGov, NASA copyright policy page or JPL Image Use Policy.)
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