Feniks No. 28L (956)
Re-entered 22 Feb 1983Feniks No. 28L (956) (NORAD 13784, COSPAR 1983-007A) was a SU satellite that re-entered Earth's atmosphere on 22 Feb 1983, launched on 6 Feb 1983 on the Feniks No. 956 mission. It was operated by GUKOS as part of the Feniks programme. The spacecraft was built by TSSKB on the Yantar'-2K bus, with a mass of 2,886 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 Feniks No. 28L (956)?
Feniks No. 28L (956) re-entered Earth's atmosphere on 22 Feb 1983, ending a mission that began with its launch in 1983. Objects in low orbits are gradually slowed by atmospheric drag until they fall back and burn up on re-entry.
When did Feniks No. 28L (956) re-enter the atmosphere?
Feniks No. 28L (956) re-entered on 22 Feb 1983, according to Orbital Radar's historical catalogue records.
Who operated and built Feniks No. 28L (956)?
Feniks No. 28L (956) was operated by GUKOS and built by TSSKB (SU).