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🛰️ SATELLITE · HISTORICAL RECORD

Gektor No. 19L

Re-entered 14 Apr 1971

Gektor No. 19L (NORAD 5108, COSPAR 1971-026A) was a SU satellite that re-entered Earth's atmosphere on 14 Apr 1971, launched on 2 Apr 1971 on the Zenit-2M mission. It was operated by GUKOSR as part of the Zenit-2M programme. The spacecraft was built by TSKBE3 on the Zenit-2M bus, with a mass of 2,200 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.

1971
launched
1971
re-entered
0
years on orbit
2,200
kg mass

Lifecycle

Launched2 Apr 1971 · on the Zenit-2M mission
Operational14 Apr 1971 · entered service
Retired14 Apr 1971 · end of operational service
Re-entered14 Apr 1971 · atmospheric re-entry — object destroyed

Specifications

NORAD ID5108
COSPAR1971-026A
TypeSatellite
OperatorGUKOSR
Country / StateSU
ManufacturerTSKBE3
BusZenit-2M
Mass2,200 kg
ProgrammeZenit-2M
CategoryIMG
OrbitLEO (LLEO/I)
Altitude212 × 227 km
Inclination81.3°

Frequently asked questions

What happened to Gektor No. 19L?

Gektor No. 19L re-entered Earth's atmosphere on 14 Apr 1971, ending a mission that began with its launch in 1971. Objects in low orbits are gradually slowed by atmospheric drag until they fall back and burn up on re-entry.

When did Gektor No. 19L re-enter the atmosphere?

Gektor No. 19L re-entered on 14 Apr 1971, according to Orbital Radar's historical catalogue records.

Who operated and built Gektor No. 19L?

Gektor No. 19L was operated by GUKOSR and built by TSKBE3 (SU).

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