Rocket body · NORAD 17481 · COSPAR 1987-012B
M-3S2 R/B
- Operator Japan
- Constellation —
- Country Japan
Altitude now
—
object decayed
Velocity
—
Inclination
31.07°
Period
87.6 min
87.6 min
Perigee
154km
Apogee
156km
orbit unavailableNo orbital element set on file — decayed 28 Jun 1997.· Metadata updated 9 h ago
Live position
Live position
Live position unavailable — this object re-entered the atmosphere on 28 Jun 1997 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
- 2.8 m²
CelesTrak groups
Not listed in any CelesTrak group.
Aliases
- M-3S2 R/BCelestrak Satcat
Ownership
Operator & country
- Operator
- —
- SATCAT owner code
- JPN · Japan
- Country
- Japan JP
Launch
Launch
- Launch date
- 05 Feb 1987
- COSPAR launch id
- 1987-012
- Launch site
- Uchinoura Space Center
Objects from the same launch · 9
- ASTRO-C DEB18229DebrisDecayed
- ASTRO-C DEB18238DebrisDecayed
- ASTRO-C DEB18407DebrisDecayed
- ASTRO-C DEB18408DebrisDecayed
- ASTRO-C DEB18409DebrisDecayed
- ASTRO-C DEB18523DebrisDecayed
- ASTRO-C DEB18682DebrisDecayed
- ASTRO-C DEB18927DebrisDecayed
- GINGA (ASTRO-C)17480PayloadDecayed
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
- 17481
- COSPAR / international designator
- 1987-012B
- SatelliteIndex id
- sat_01M28X3JNW3451HHBKNAPJ2N9P
- Canonical slug
- m-3s2-r-b-17481
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.