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OV-105

Re-entered 7 Jun 2002

OV-105 (NORAD 27440, COSPAR 2002-028A) was a US satellite that re-entered Earth's atmosphere on 7 Jun 2002, launched on 5 Jun 2002 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 98,660 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.

2002
launched
2002
re-entered
0
years on orbit
98,660
kg mass

Lifecycle

Launched5 Jun 2002 · on the OV-105 ISS mission
Operational19 Jun 2002 · entered service
Retired19 Jun 2002 · end of operational service
Re-entered7 Jun 2002 · atmospheric re-entry — object destroyed

Specifications

NORAD ID27440
COSPAR2002-028A
TypeSatellite
OperatorJSC
Country / StateUS
ManufacturerBNAP
BusSTS OV
Mass98,660 kg (86,750 kg dry)
ProgrammeSTS
CategorySS
OrbitLEO (LLEO/I)
Altitude381 × 389 km
Inclination51.6°

Frequently asked questions

What happened to OV-105?

OV-105 re-entered Earth's atmosphere on 7 Jun 2002, ending a mission that began with its launch in 2002. 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 7 Jun 2002, 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).

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