Debris object · NORAD 32012 · COSPAR 2006-037J
H-2A DEB
- Operator Japan
- Constellation —
- Country Japan
Altitude now
—
object decayed
Velocity
—
Inclination
97.27°
Period
91.3 min
91.3 min
Perigee
326km
Apogee
352km
orbit unavailableNo orbital element set on file — decayed 14 Aug 2007.· Metadata updated 9 h ago
Live position
Live position
Live position unavailable — this object re-entered the atmosphere on 14 Aug 2007 and is no longer tracked.
Mission
Mission & classification
- Mission type derived
- Debris
- Object type
- Debris
- SATCAT ops status
- Decayed [D]
- Radar cross-section
- 0.0 m²
CelesTrak groups
Not listed in any CelesTrak group.
Aliases
- H-2A DEBCelestrak 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 DEB32013DebrisDecayed
- H-2A DEB32014DebrisDecayed
- H-2A DEB32015DebrisDecayed
- H-2A DEB32016DebrisDecayed
- H-2A DEB32017DebrisDecayed
- IGS 3A29393PayloadDecayed
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
- 32012
- COSPAR / international designator
- 2006-037J
- SatelliteIndex id
- sat_01M28X3JRC2VCNFE403FNKZBPC
- Canonical slug
- h-2a-deb-32012
Orbit class, mission type and constellation membership are derived by SatelliteIndex (Debris) — see the methodology. Positions are propagated estimates, not tracking measurements; never use them for conjunction assessment.