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OV-105

Re-entered 2 Dec 2000

OV-105 (NORAD 26630, COSPAR 2000-078A) was a US satellite that re-entered Earth's atmosphere on 2 Dec 2000, launched on 1 Dec 2000 on the OV-105 ISS mission. It was operated by JSC as part of the STS programme. The spacecraft was built by BNAP on the STS OV bus, with a mass of 95,600 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
2000
re-entered
0
years on orbit
95,600
kg mass

Lifecycle

Launched1 Dec 2000 · on the OV-105 ISS mission
Operational11 Dec 2000 · entered service
Retired11 Dec 2000 · end of operational service
Re-entered2 Dec 2000 · atmospheric re-entry — object destroyed

Specifications

NORAD ID26630
COSPAR2000-078A
TypeSatellite
OperatorJSC
Country / StateUS
ManufacturerBNAP
BusSTS OV
Mass95,600 kg (86,660 kg dry)
ProgrammeSTS
CategorySS
OrbitLEO (LLEO/I)
Altitude207 × 322 km
Inclination51.6°

Frequently asked questions

What happened to OV-105?

OV-105 re-entered Earth's atmosphere on 2 Dec 2000, 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 OV-105 re-enter the atmosphere?

OV-105 re-entered on 2 Dec 2000, according to Orbital Radar's historical catalogue records.

Who operated and built OV-105?

OV-105 was operated by JSC and built by BNAP (US).

Launched together

Floating Potential ProbeRe-entered 2000
Historical record from the Orbital Radar satellite archive. Sources & methodology: data sources. Accessed 2026-09-06.