Mission Design

	Eros Orbits and Maneuvers
		• Design of Eros spacecraft orbits and preliminary orbit correction maneuvers courtesy NASA/JPL Navigation
		• Design of heliocentric spacecraft orbits and final orbit correction maneuvers courtesy JHU/APL
		• 14 Feb 00 - 1 Mar 01
	Diagrams
		5-km (3-mile) Altitude Flyby on October 26, 2000: JPEG Initial Approach to Eros: Full size , 1/2 size Rendezvous to Orbit Insertion GIF All mission trajectory events: Simple , Detailed
	Trajectory Data Excel (.xls) format -- !! Updated through last contact !! • All spacecraft and asteroid orbit data provided by NASA/JPL Navigation
		• trajdata_to_EOM.xls 18 Feb 96 - 1 Mar 01; Launch to End of Mission 21.4M • OIM_onward_eqtr.xls 14 Feb 00 - 1 Mar 01; 100 records/day Eros equator and prime meridian of date 17.4M • OIM_onward_spos.xls 14 Feb 00 - 1 Mar 01; 100 records/day Eros Sun Plane-of-Sky (view from the Sun) 17.4M
	Trajectory Animations NEW! --- updated 31 Jan 01 ---

Orbital Elements Table Contains Keplerian orbital elements in Earth Mean Ecliptic of J2000 from launch to Eros Rendezvous For Eros Orbital Phase data, see Download Trajectory Data. above HTML Excel (.xls) Propulsive Event Summary Summarizes each past propulsive event HTML Excel (.xls)

Contact: Jim McAdams, APL