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Zenit-4 No. 30L

Re-entered 9 Jun 1967

Zenit-4 No. 30L (NORAD 2827, COSPAR 1967-054A) was a SU satellite that re-entered Earth's atmosphere on 9 Jun 1967, launched on 1 Jun 1967 on the Zenit-4 No. 30 mission. It was operated by TSUKOS as part of the Zenit-4 programme. The spacecraft was built by TSKBE3 on the Zenit-4 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.

1967
launched
1967
re-entered
0
years on orbit
2,200
kg mass

Lifecycle

Launched1 Jun 1967 · on the Zenit-4 No. 30 mission
Operational9 Jun 1967 · entered service
Retired9 Jun 1967 · end of operational service
Re-entered9 Jun 1967 · atmospheric re-entry — object destroyed

Specifications

NORAD ID2827
COSPAR1967-054A
TypeSatellite
OperatorTSUKOS
Country / StateSU
ManufacturerTSKBE3
BusZenit-4
Mass2,200 kg
ProgrammeZenit-4
CategoryIMG
OrbitLEO (LLEO/I)
Altitude191 × 275 km
Inclination51.7°

Frequently asked questions

What happened to Zenit-4 No. 30L?

Zenit-4 No. 30L re-entered Earth's atmosphere on 9 Jun 1967, ending a mission that began with its launch in 1967. Objects in low orbits are gradually slowed by atmospheric drag until they fall back and burn up on re-entry.

When did Zenit-4 No. 30L re-enter the atmosphere?

Zenit-4 No. 30L re-entered on 9 Jun 1967, according to Orbital Radar's historical catalogue records.

Who operated and built Zenit-4 No. 30L?

Zenit-4 No. 30L was operated by TSUKOS and built by TSKBE3 (SU).

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