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🛰️ SATELLITE · HISTORICAL RECORD

Fram No. 23L

Re-entered 11 May 1983

Fram No. 23L (NORAD 14044, COSPAR 1983-040A) was a SU satellite that re-entered Earth's atmosphere on 11 May 1983, launched on 28 Apr 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.

1983
launched
1983
re-entered
0
years on orbit
2,455
kg mass

Lifecycle

Launched28 Apr 1983 · on the Fram mission
Operational11 May 1983 · entered service
Retired11 May 1983 · end of operational service
Re-entered11 May 1983 · atmospheric re-entry — object destroyed

Specifications

NORAD ID14044
COSPAR1983-040A
TypeSatellite
OperatorPRIR
Country / StateSU
ManufacturerTSSKB
BusFram
Mass2,455 kg
ProgrammeFram
CategoryIMG
OrbitLEO (LLEO/I)
Altitude209 × 244 km
Inclination82.3°

Frequently asked questions

What happened to Fram No. 23L?

Fram No. 23L re-entered Earth's atmosphere on 11 May 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. 23L re-enter the atmosphere?

Fram No. 23L re-entered on 11 May 1983, according to Orbital Radar's historical catalogue records.

Who operated and built Fram No. 23L?

Fram No. 23L 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.