Rocket body · NORAD 19823 · COSPAR 1989-016B
M-3S2 R/B(1)
- Operator Japan
- Constellation —
- Country Japan
Altitude now
—
object decayed
Velocity
—
Inclination
74.54°
Period
87.7 min
87.7 min
Perigee
147km
Apogee
172km
orbit unavailableNo orbital element set on file — decayed 04 Apr 1989.· Metadata updated 9 h ago
Live position
Live position
Live position unavailable — this object re-entered the atmosphere on 04 Apr 1989 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
- 6.3 m²
CelesTrak groups
Not listed in any CelesTrak group.
Aliases
- M-3S2 R/B(1)Celestrak Satcat
Ownership
Operator & country
- Operator
- —
- SATCAT owner code
- JPN · Japan
- Country
- Japan JP
Launch
Launch
- Launch date
- 21 Feb 1989
- COSPAR launch id
- 1989-016
- Launch site
- Uchinoura Space Center
Objects from the same launch · 13
- M-3S2 DEB19841DebrisDecayed
- M-3S2 DEB19842DebrisDecayed
- M-3S2 DEB19843DebrisDecayed
- M-3S2 DEB19844DebrisDecayed
- M-3S2 DEB19845DebrisDecayed
- M-3S2 DEB19889DebrisDecayed
- M-3S2 DEB19952DebrisDecayed
- M-3S2 DEB19962DebrisDecayed
- M-3S2 DEB19963DebrisDecayed
- M-3S2 DEB20021DebrisDecayed
- M-3S2 DEB20034DebrisDecayed
- AKEBONO (EXOS-D)19822PayloadDecayed
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
- 19823
- COSPAR / international designator
- 1989-016B
- SatelliteIndex id
- sat_01M28X3JP922NG7PYWKE2KHCMS
- Canonical slug
- m-3s2-r-b-1-19823
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.