Rocket body · NORAD 29394 · COSPAR 2006-037B
H-2A R/B
- Operator Japan
- Constellation —
- Country Japan
Altitude now
—
object decayed
Velocity
—
Inclination
97.40°
Period
87.5 min
87.5 min
Perigee
146km
Apogee
155km
orbit unavailableNo orbital element set on file — decayed 16 Feb 2012.· Metadata updated 9 h ago
Live position
Live position
Live position unavailable — this object re-entered the atmosphere on 16 Feb 2012 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
- 17.3 m²
CelesTrak groups
Not listed in any CelesTrak group.
Aliases
- H-2A R/BCelestrak Satcat
Ownership
Operator & country
- Operator
- —
- SATCAT owner code
- JPN · Japan
- Country
- Japan JP
Launch
Launch
- Launch date
- 11 Sept 2006
- COSPAR launch id
- 2006-037
- Launch site
- Tanegashima Space Center
Objects from the same launch · 13
- H-2A DEB29395DebrisDecayed
- H-2A DEB29396DebrisDecayed
- H-2A DEB29493DebrisDecayed
- H-2A DEB32009DebrisDecayed
- H-2A DEB32010DebrisDecayed
- H-2A DEB32011DebrisDecayed
- H-2A DEB32012DebrisDecayed
- H-2A DEB32013DebrisDecayed
- H-2A DEB32014DebrisDecayed
- H-2A DEB32015DebrisDecayed
- H-2A DEB32016DebrisDecayed
- H-2A DEB32017DebrisDecayed
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
- 29394
- COSPAR / international designator
- 2006-037B
- SatelliteIndex id
- sat_01M28X3JQYTTX7QCSDSBM8RW0V
- Canonical slug
- h-2a-r-b-29394
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.