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Gektor-Priroda No. 103L

Re-entered 25 Jun 1979

Gektor-Priroda No. 103L (NORAD 11399, COSPAR 1979-054A) was a SU satellite that re-entered Earth's atmosphere on 25 Jun 1979, launched on 12 Jun 1979 on the Gektor-Priroda mission. It was operated by PRIR as part of the Gektor-Priroda programme. The spacecraft was built by TSSKB 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.

1979
launched
1979
re-entered
0
years on orbit
2,200
kg mass

Lifecycle

Launched12 Jun 1979 · on the Gektor-Priroda mission
Operational25 Jun 1979 · entered service
Retired25 Jun 1979 · end of operational service
Re-entered25 Jun 1979 · atmospheric re-entry — object destroyed

Specifications

NORAD ID11399
COSPAR1979-054A
TypeSatellite
OperatorPRIR
Country / StateSU
ManufacturerTSSKB
BusZenit-2M
Mass2,200 kg
ProgrammeGektor-Priroda
CategoryIMG
OrbitLEO (LLEO/I)
Altitude212 × 233 km
Inclination81.4°

Frequently asked questions

What happened to Gektor-Priroda No. 103L?

Gektor-Priroda No. 103L re-entered Earth's atmosphere on 25 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 Gektor-Priroda No. 103L re-enter the atmosphere?

Gektor-Priroda No. 103L re-entered on 25 Jun 1979, according to Orbital Radar's historical catalogue records.

Who operated and built Gektor-Priroda No. 103L?

Gektor-Priroda No. 103L was operated by PRIR and built by TSSKB (SU).

Launched together

Nauka 33KS No. 1LRe-entered 1979
Historical record from the Orbital Radar satellite archive. Sources & methodology: data sources. Accessed 2026-09-06.