Debris object · NORAD 53336 · COSPAR 2018-084EJ
H-2A DEB
- Operator Japan
- Constellation —
- Country Japan
Altitude now
—
object decayed
Velocity
—
Inclination
97.80°
Period
92.4 min
92.4 min
Perigee
361km
Apogee
419km
orbit unavailableNo orbital element set on file — decayed 12 Sept 2022.· Metadata updated 8 h ago
Live position
Live position
Live position unavailable — this object re-entered the atmosphere on 12 Sept 2022 and is no longer tracked.
Mission
Mission & classification
- Mission type derived
- Debris
- Object type
- Debris
- SATCAT ops status
- Decayed [D]
- Radar cross-section
- —
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
- 29 Oct 2018
- COSPAR launch id
- 2018-084
- Launch site
- Tanegashima Space Center
Objects from the same launch · 40+
- H-2A DEB43673DebrisDecayed
- H-2A DEB43674DebrisDecayed
- H-2A DEB43675DebrisDecayed
- H-2A DEB44051DebrisDecayed
- H-2A DEB44052DebrisDecayed
- H-2A DEB44053DebrisDecayed
- H-2A DEB44054DebrisDecayed
- H-2A DEB44620DebrisDecayed
- H-2A DEB46181DebrisDecayed
- H-2A DEB46182DebrisDecayed
- H-2A DEB46183DebrisDecayed
- H-2A DEB46184DebrisDecayed
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
- 53336
- COSPAR / international designator
- 2018-084EJ
- SatelliteIndex id
- sat_01M28X3JW87J8A5B6VQ30W7KRG
- Canonical slug
- h-2a-deb-53336
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.