Fram No. 2L
Re-entered 2 Jun 1976Fram No. 2L (NORAD 8856, COSPAR 1976-046A) was a SU satellite that re-entered Earth's atmosphere on 2 Jun 1976, launched on 21 May 1976 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. 2L?
Fram No. 2L re-entered Earth's atmosphere on 2 Jun 1976, ending a mission that began with its launch in 1976. Objects in low orbits are gradually slowed by atmospheric drag until they fall back and burn up on re-entry.
When did Fram No. 2L re-enter the atmosphere?
Fram No. 2L re-entered on 2 Jun 1976, according to Orbital Radar's historical catalogue records.
Who operated and built Fram No. 2L?
Fram No. 2L was operated by PRIR and built by TSSKB (SU).