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IS-M GVM No. 002

Re-entered 8 Sep 1969

IS-M GVM No. 002 (NORAD 4058, COSPAR 1969-066A) was a SU satellite that re-entered Earth's atmosphere on 8 Sep 1969, launched on 6 Aug 1969 on the IS-M GVM mission. It was operated by PKO as part of the IS 5V91M programme. The spacecraft was built by TSKBM/KB1 on the IS bus, with a mass of 1,400 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.

1969
launched
1969
re-entered
0
years on orbit
1,400
kg mass

Lifecycle

Launched6 Aug 1969 · on the IS-M GVM mission
Operational8 Sep 1969 · entered service
Retired8 Sep 1969 · end of operational service
Re-entered8 Sep 1969 · atmospheric re-entry — object destroyed

Specifications

NORAD ID4058
COSPAR1969-066A
TypeSatellite
OperatorPKO
Country / StateSU
ManufacturerTSKBM/KB1
BusIS
Mass1,400 kg
ProgrammeIS 5V91M
CategoryTARG
OrbitLEO (LLEO/I)
Altitude142 × 495 km
Inclination62.2°

Frequently asked questions

What happened to IS-M GVM No. 002?

IS-M GVM No. 002 re-entered Earth's atmosphere on 8 Sep 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 IS-M GVM No. 002 re-enter the atmosphere?

IS-M GVM No. 002 re-entered on 8 Sep 1969, according to Orbital Radar's historical catalogue records.

Who operated and built IS-M GVM No. 002?

IS-M GVM No. 002 was operated by PKO and built by TSKBM/KB1 (SU).

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