Fram No. 24L
Re-entered 16 Sep 1983Fram No. 24L (NORAD 14320, COSPAR 1983-092A) was a SU satellite that re-entered Earth's atmosphere on 16 Sep 1983, launched on 3 Sep 1983 on the Fram mission. It was operated by PRIR as part of the Fram programme. The spacecraft was built by TSSKB on the Fram bus, with a mass of 2,455 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 Fram No. 24L?
Fram No. 24L re-entered Earth's atmosphere on 16 Sep 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 Fram No. 24L re-enter the atmosphere?
Fram No. 24L re-entered on 16 Sep 1983, according to Orbital Radar's historical catalogue records.
Who operated and built Fram No. 24L?
Fram No. 24L was operated by PRIR and built by TSSKB (SU).