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Strela-1 GVM

Re-entered 15 Sep 1968

Strela-1 GVM (NORAD 1089, COSPAR 1965-011A) was a SU satellite that re-entered Earth's atmosphere on 15 Sep 1968, launched on 21 Feb 1965 on the Strela-1 mission. It was operated by OKB10 as part of the Strela-1 programme. The spacecraft was built by OKB10 on the Strela-1 11F610 bus, with a mass of 50 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.

1965
launched
1968
re-entered
3
years on orbit
50
kg mass

Lifecycle

Launched21 Feb 1965 · on the Strela-1 mission
Operational1 Jan 1965 · entered service
Retired1 Jan 1965 · end of operational service
Re-entered15 Sep 1968 · atmospheric re-entry — object destroyed

Specifications

NORAD ID1089
COSPAR1965-011A
TypeSatellite
OperatorOKB10
Country / StateSU
ManufacturerOKB10
BusStrela-1 11F610
Mass50 kg
ProgrammeStrela-1
CategoryCOM
OrbitLEO (LEO/I)
Altitude260 × 1,711 km
Inclination56.0°

Frequently asked questions

What happened to Strela-1 GVM?

Strela-1 GVM re-entered Earth's atmosphere on 15 Sep 1968, ending a mission that began with its launch in 1965. Objects in low orbits are gradually slowed by atmospheric drag until they fall back and burn up on re-entry.

When did Strela-1 GVM re-enter the atmosphere?

Strela-1 GVM re-entered on 15 Sep 1968, according to Orbital Radar's historical catalogue records.

Who operated and built Strela-1 GVM?

Strela-1 GVM was operated by OKB10 and built by OKB10 (SU).

Launched together

Strela-1 GVMRe-entered 1968Strela-1 GVMRe-entered 1967
Historical record from the Orbital Radar satellite archive. Sources & methodology: data sources. Accessed 2026-09-06.