TKS GVM

Re-entered 16 Jun 1979

TKS GVM (NORAD 11365, COSPAR 1979-042D) was a SU satellite that re-entered Earth's atmosphere on 16 Jun 1979, launched on 22 May 1979 on the TKS VA No. 0102A mission. It was operated by ZIKH as part of the TKS programme. The spacecraft was built by ZIKH on the TKS GVM bus, with a mass of 10,000 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.

1979

launched

1979

re-entered

years on orbit

10,000

kg mass

Lifecycle

Launched22 May 1979 · on the TKS VA No. 0102A mission

Operational22 May 1979 · entered service

Retired22 May 1979 · end of operational service

Re-entered16 Jun 1979 · atmospheric re-entry — object destroyed

Specifications

NORAD ID11365

COSPAR1979-042D

TypeSatellite

OperatorZIKH

Country / StateSU

ManufacturerZIKH

BusTKS GVM

Mass10,000 kg

ProgrammeTKS

CategorySS

OrbitLEO (LLEO/I)

Altitude190 × 220 km

Inclination51.6°

Frequently asked questions

What happened to TKS GVM?

TKS GVM re-entered Earth's atmosphere on 16 Jun 1979, ending a mission that began with its launch in 1979. Objects in low orbits are gradually slowed by atmospheric drag until they fall back and burn up on re-entry.

When did TKS GVM re-enter the atmosphere?

TKS GVM re-entered on 16 Jun 1979, according to Orbital Radar's historical catalogue records.

Who operated and built TKS GVM?

TKS GVM was operated by ZIKH and built by ZIKH (SU).

Launched together

TKS VA No. 0102ARe-entered 1979 TKS VA No. 0102Re-entered 1979

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

Browse the live satellite directory → Re-entered satellites archive → Launch record: TKS VA No. 0102A → What is space debris? →