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Yenisey No. 2L

Re-entered 20 Apr 2001

Yenisey No. 2L (NORAD 26538, COSPAR 2000-056A) was a RU satellite that re-entered Earth's atmosphere on 20 Apr 2001, launched on 25 Sep 2000 on the Yenisey mission. It was operated by VKSR as part of the Orlets programme. The spacecraft was built by TSSKBP on the Orlets-2 bus, with a mass of 4,150 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.

2000
launched
2001
re-entered
1
year on orbit
4,150
kg mass

Lifecycle

Launched25 Sep 2000 · on the Yenisey mission
Operational20 Apr 2001 · entered service
Retired20 Apr 2001 · end of operational service
Re-entered20 Apr 2001 · atmospheric re-entry — object destroyed

Specifications

NORAD ID26538
COSPAR2000-056A
TypeSatellite
OperatorVKSR
Country / StateRU
ManufacturerTSSKBP
BusOrlets-2
Mass4,150 kg (2,350 kg dry)
ProgrammeOrlets
CategoryIMG
OrbitLEO (LLEO/I)
Altitude210 × 335 km
Inclination64.8°

Frequently asked questions

What happened to Yenisey No. 2L?

Yenisey No. 2L re-entered Earth's atmosphere on 20 Apr 2001, ending a mission that began with its launch in 2000. Objects in low orbits are gradually slowed by atmospheric drag until they fall back and burn up on re-entry.

When did Yenisey No. 2L re-enter the atmosphere?

Yenisey No. 2L re-entered on 20 Apr 2001, according to Orbital Radar's historical catalogue records.

Who operated and built Yenisey No. 2L?

Yenisey No. 2L was operated by VKSR and built by TSSKBP (RU).

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