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Zenit-4MT No. 2L

Re-entered 25 Jul 1972

Zenit-4MT No. 2L (NORAD 6105, COSPAR 1972-055A) was a SU satellite that re-entered Earth's atmosphere on 25 Jul 1972, launched on 13 Jul 1972 on the Zenit-4MT mission. It was operated by TSKBE3 as part of the Orion programme. The spacecraft was built by TSKBE3 on the Zenit-4MT 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.

1972
launched
1972
re-entered
0
years on orbit
2,200
kg mass

Lifecycle

Launched13 Jul 1972 · on the Zenit-4MT mission
Operational25 Jul 1972 · entered service
Retired25 Jul 1972 · end of operational service
Re-entered25 Jul 1972 · atmospheric re-entry — object destroyed

Specifications

NORAD ID6105
COSPAR1972-055A
TypeSatellite
OperatorTSKBE3
Country / StateSU
ManufacturerTSKBE3
BusZenit-4MT
Mass2,200 kg
ProgrammeOrion
CategoryIMG
OrbitLEO (LLEO/I)
Altitude200 × 263 km
Inclination65.4°

Frequently asked questions

What happened to Zenit-4MT No. 2L?

Zenit-4MT No. 2L re-entered Earth's atmosphere on 25 Jul 1972, ending a mission that began with its launch in 1972. Objects in low orbits are gradually slowed by atmospheric drag until they fall back and burn up on re-entry.

When did Zenit-4MT No. 2L re-enter the atmosphere?

Zenit-4MT No. 2L re-entered on 25 Jul 1972, according to Orbital Radar's historical catalogue records.

Who operated and built Zenit-4MT No. 2L?

Zenit-4MT No. 2L 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.