Rocket body · NORAD 23524 · COSPAR 1995-011D
HIMAWARI-5 AKM
- Operator Japan
- Constellation —
- Country Japan
Altitude now
—
no element set
Velocity
—
Inclination
13.58°
Period
23.7 h
1,422.2 min
Perigee
34,607km
Apogee
36,421km
orbit unavailableNo orbital element set on file.· Metadata updated 10 h ago
Live position
Live position
Live position unavailable — no public orbital element set exists for this object (it may be classified, untracked or too small to catalogue).
Mission
Mission & classification
- Mission type derived
- Rocket body
- Object type
- Rocket body
- Radar cross-section
- 0.5 m²
CelesTrak groups
Not listed in any CelesTrak group.
Aliases
- HIMAWARI-5 AKMCelestrak Satcat
Ownership
Operator & country
- Operator
- —
- SATCAT owner code
- JPN · Japan
- Country
- Japan JP
Launch
Launch
- Launch date
- 18 Mar 1995
- COSPAR launch id
- 1995-011
- Launch site
- Tanegashima Space Center
Objects from the same launch · 9
- SFU DEB23569DebrisDecayed
- SFU DEB23570DebrisDecayed
- SFU DEB23593DebrisDecayed
- SFU DEB23771DebrisDecayed
- SFU DEB23772DebrisDecayed
- SFU23521PayloadDecayed
- HIMAWARI-5 (GMS-5)23522PayloadUnknown
- H-2 R/B(2)23523Rocket bodyInactive
- H-2 R/B(1)23525Rocket bodyDecayed
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
- 23524
- COSPAR / international designator
- 1995-011D
- SatelliteIndex id
- sat_01M28X3JPYTMBEXACP2PNHK1N3
- Canonical slug
- himawari-5-akm-23524
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.