Progress 7K-TGM No. 247

Re-entered 4 Feb 2003

Progress 7K-TGM No. 247 (NORAD 27681, COSPAR 2003-006A) was a RU satellite that re-entered Earth's atmosphere on 4 Feb 2003, launched on 2 Feb 2003 on the Progress M No. 247 mission. It was operated by RKKE as part of the Progress M programme. The spacecraft was built by PROGT on the 7K-TGM bus, with a mass of 7,230 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.

2003

launched

2003

re-entered

years on orbit

7,230

kg mass

Lifecycle

Launched2 Feb 2003 · on the Progress M No. 247 mission

Operational28 Aug 2003 · entered service

Retired28 Aug 2003 · end of operational service

Re-entered4 Feb 2003 · atmospheric re-entry — object destroyed

Specifications

NORAD ID27681

COSPAR2003-006A

TypeSatellite

OperatorRKKE

Country / StateRU

ManufacturerPROGT

Bus7K-TGM

Mass7,230 kg (4,600 kg dry)

ProgrammeProgress M

CategorySS

OrbitLEO (LLEO/I)

Altitude271 × 304 km

Inclination51.6°

Frequently asked questions

What happened to Progress 7K-TGM No. 247?

Progress 7K-TGM No. 247 re-entered Earth's atmosphere on 4 Feb 2003, ending a mission that began with its launch in 2003. Objects in low orbits are gradually slowed by atmospheric drag until they fall back and burn up on re-entry.

When did Progress 7K-TGM No. 247 re-enter the atmosphere?

Progress 7K-TGM No. 247 re-entered on 4 Feb 2003, according to Orbital Radar's historical catalogue records.

Who operated and built Progress 7K-TGM No. 247?

Progress 7K-TGM No. 247 was operated by RKKE and built by PROGT (RU).

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

Browse the live satellite directory → Re-entered satellites archive → Launch record: Progress M No. 247 → What is space debris? →