Zenit-4M No. 2L
Re-entered 5 Feb 1969Zenit-4M No. 2L (NORAD 3667, COSPAR 1969-008A) was a SU satellite that re-entered Earth's atmosphere on 5 Feb 1969, launched on 23 Jan 1969 on the Zenit-4M mission. It was operated by TSKBE3 as part of the Zenit-4M programme. The spacecraft was built by TSKBE3 on the Zenit-4M bus, with a mass of 2,200 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 Zenit-4M No. 2L?
Zenit-4M No. 2L re-entered Earth's atmosphere on 5 Feb 1969, ending a mission that began with its launch in 1969. Objects in low orbits are gradually slowed by atmospheric drag until they fall back and burn up on re-entry.
When did Zenit-4M No. 2L re-enter the atmosphere?
Zenit-4M No. 2L re-entered on 5 Feb 1969, according to Orbital Radar's historical catalogue records.
Who operated and built Zenit-4M No. 2L?
Zenit-4M No. 2L was operated by TSKBE3 and built by TSKBE3 (SU).