Trajectory & orbital insertion · playback
Orbits are real (live SGP4) — press play to sweep the deployed group forward along their planes. Ascent path is a representation; true ascent telemetry isn’t public.
Provider
China Aerospace Science and Technology Corporation
Provider type
Government
Orbit
LEO
Mission type
Navigation
Launch site
China
Date
Mon, 23 Oct 2006 23:34:00 GMT
Orbital launch #
#4800 ever
Mission
It was announced that the two satellites had a design life of at least two years, and would be used to probe the space environment, radiation and its effects, record space physical environment parameters, and conduct other related space experiments.
Deployed payloads · 3