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🛰️ SATELLITE · HISTORICAL RECORD

Zenit-2M No. 7L

Re-entered 15 Dec 1969

Zenit-2M No. 7L (NORAD 4262, COSPAR 1969-104A) was a SU satellite that re-entered Earth's atmosphere on 15 Dec 1969, launched on 3 Dec 1969 on the Zenit-2M mission. It was operated by TSKBE3 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.

1969
launched
1969
re-entered
0
years on orbit
2,200
kg mass

Lifecycle

Launched3 Dec 1969 · on the Zenit-2M mission
Operational15 Dec 1969 · entered service
Retired15 Dec 1969 · end of operational service
Re-entered15 Dec 1969 · atmospheric re-entry — object destroyed

Specifications

NORAD ID4262
COSPAR1969-104A
TypeSatellite
OperatorTSKBE3
Country / StateSU
ManufacturerTSKBE3
BusZenit-2M
Mass2,200 kg
ProgrammeZenit-2M
CategoryIMG
OrbitLEO (LLEO/I)
Altitude198 × 252 km
Inclination65.4°

Frequently asked questions

What happened to Zenit-2M No. 7L?

Zenit-2M No. 7L re-entered Earth's atmosphere on 15 Dec 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 Zenit-2M No. 7L re-enter the atmosphere?

Zenit-2M No. 7L re-entered on 15 Dec 1969, according to Orbital Radar's historical catalogue records.

Who operated and built Zenit-2M No. 7L?

Zenit-2M No. 7L was operated by TSKBE3 and built by TSKBE3 (SU).

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