Shenzhou 3 orbital module
Re-entered 12 Nov 2002Shenzhou 3 orbital module (NORAD 27408, COSPAR 2002-014C) was a CN satellite that re-entered Earth's atmosphere on 12 Nov 2002, launched on 25 Mar 2002 on the Shenzhou 3 Fanhui Cang mission. It was operated by CMSEO as part of the Shenzhou OM programme. The spacecraft was built by CALT on the Shenzhou OM bus, with a mass of 1,700 kg. Like most satellites in low orbits, it was gradually slowed by atmospheric drag until re-entry. Historical record from Orbital Radar's satellite archive, cross-referenced with the live satellite catalogue.
Lifecycle
Specifications
Frequently asked questions
What happened to Shenzhou 3 orbital module?
Shenzhou 3 orbital module re-entered Earth's atmosphere on 12 Nov 2002, ending a mission that began with its launch in 2002. Objects in low orbits are gradually slowed by atmospheric drag until they fall back and burn up on re-entry.
When did Shenzhou 3 orbital module re-enter the atmosphere?
Shenzhou 3 orbital module re-entered on 12 Nov 2002, according to Orbital Radar's historical catalogue records.
Who operated and built Shenzhou 3 orbital module?
Shenzhou 3 orbital module was operated by CMSEO and built by CALT (CN).