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🛰️ SATELLITE · HISTORICAL RECORD

Fram No. 14L

Re-entered 28 Jul 1980

Fram No. 14L (NORAD 11894, COSPAR 1980-061A) was a SU satellite that re-entered Earth's atmosphere on 28 Jul 1980, launched on 15 Jul 1980 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.

1980
launched
1980
re-entered
0
years on orbit
2,455
kg mass

Lifecycle

Launched15 Jul 1980 · on the Fram mission
Operational28 Jul 1980 · entered service
Retired28 Jul 1980 · end of operational service
Re-entered28 Jul 1980 · atmospheric re-entry — object destroyed

Specifications

NORAD ID11894
COSPAR1980-061A
TypeSatellite
OperatorPRIR
Country / StateSU
ManufacturerTSSKB
BusFram
Mass2,455 kg
ProgrammeFram
CategoryIMG
OrbitLEO (LLEO/I)
Altitude209 × 233 km
Inclination82.3°

Frequently asked questions

What happened to Fram No. 14L?

Fram No. 14L re-entered Earth's atmosphere on 28 Jul 1980, ending a mission that began with its launch in 1980. Objects in low orbits are gradually slowed by atmospheric drag until they fall back and burn up on re-entry.

When did Fram No. 14L re-enter the atmosphere?

Fram No. 14L re-entered on 28 Jul 1980, according to Orbital Radar's historical catalogue records.

Who operated and built Fram No. 14L?

Fram No. 14L was operated by PRIR and built by TSSKB (SU).

Historical record from the Orbital Radar satellite archive. Sources & methodology: data sources. Accessed 2026-09-06.