EPN No. 03.0380
Re-entered 27 Jun 1982EPN No. 03.0380 (NORAD 10375, COSPAR 1977-095A) was a SU satellite that re-entered Earth's atmosphere on 27 Jun 1982, launched on 24 Sep 1977 on the EPN No. 03.0380 mission. It was operated by YUZH as part of the Okean-E programme. The spacecraft was built by YUZH on the GVM bus, with a mass of 1,800 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 EPN No. 03.0380?
EPN No. 03.0380 re-entered Earth's atmosphere on 27 Jun 1982, ending a mission that began with its launch in 1977. Objects in low orbits are gradually slowed by atmospheric drag until they fall back and burn up on re-entry.
When did EPN No. 03.0380 re-enter the atmosphere?
EPN No. 03.0380 re-entered on 27 Jun 1982, according to Orbital Radar's historical catalogue records.
Who operated and built EPN No. 03.0380?
EPN No. 03.0380 was operated by YUZH and built by YUZH (SU).