Rocket body · NORAD 29480 · COSPAR 2006-041B
M-5 R/B
- Operator Japan
- Constellation —
- Country Japan
Altitude now
—
object decayed
Velocity
—
Inclination
98.24°
Period
87.3 min
87.3 min
Perigee
132km
Apogee
145km
orbit unavailableNo orbital element set on file — decayed 20 Oct 2009.· Metadata updated 14 h ago
Live position
Live position
Live position unavailable — this object re-entered the atmosphere on 20 Oct 2009 and is no longer tracked.
Mission
Mission & classification
- Mission type derived
- Rocket body
- Object type
- Rocket body
- SATCAT ops status
- Decayed [D]
- Radar cross-section
- 7.9 m²
CelesTrak groups
Not listed in any CelesTrak group.
Aliases
- M-5 R/BCelestrak Satcat
Ownership
Operator & country
- Operator
- —
- SATCAT owner code
- JPN · Japan
- Country
- Japan JP
Launch
Launch
- Launch date
- 22 Sept 2006
- COSPAR launch id
- 2006-041
- Launch site
- Uchinoura Space Center
Objects from the same launch · 10
- M-5 DEB29481DebrisDecayed
- M-5 DEB29482DebrisDecayed
- M-5 DEB29483DebrisDecayed
- M-5 DEB29485DebrisDecayed
- M-5 DEB29490DebrisDecayed
- M-5 DEB29491DebrisDecayed
- M-5 DEB29492DebrisDecayed
- M-5 DEB31390DebrisDecayed
- HINODE (SOLAR-B)29479PayloadActive
- HIT-SAT (HO-59)29484PayloadDecayed
Change log
History
No changes recorded since first ingestion on 11 Sept 2026 18:54 UTC. Status, orbit class, name and ownership changes are logged here as sources are re-ingested.
Regulatory
UN registration
Transparency
Sources & provenance
No source is linked to this record yet — the catalogue row exists but no provenance entry has been written for it.
Field provenance
No field-level provenance recorded.
Timeline
Events
No events detected for this object yet. Launches, decays and orbit changes are generated by the derived-analytics connector.
Reference
Identifiers
- NORAD catalogue number
- 29480
- COSPAR / international designator
- 2006-041B
- SatelliteIndex id
- sat_01M28X3JQZXWENWV0EEATTWTS7
- Canonical slug
- m-5-r-b-29480
Orbit class, mission type and constellation membership are derived by SatelliteIndex (Rocket body) — see the methodology. Positions are propagated estimates, not tracking measurements; never use them for conjunction assessment.