Rocket body · NORAD 14498 · COSPAR 1983-112B
SL-4 R/B
- Operator Commonwealth of Independent States (former USSR)
- Constellation —
- Country Russia
Altitude now
—
object decayed
Velocity
—
Inclination
72.84°
Period
87.4 min
87.4 min
Perigee
137km
Apogee
152km
orbit unavailableNo orbital element set on file — decayed 22 Nov 1983.· Metadata updated 15 h ago
Live position
Live position
Live position unavailable — this object re-entered the atmosphere on 22 Nov 1983 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
- —
CelesTrak groups
Not listed in any CelesTrak group.
Aliases
- SL-4 R/BCelestrak Satcat
Ownership
Operator & country
- Operator
- —
- SATCAT owner code
- CIS · Commonwealth of Independent States (former USSR)
- Country
- Russia RU
Launch
Launch
- Launch date
- 17 Nov 1983
- COSPAR launch id
- 1983-112
- Launch site
- Plesetsk Cosmodrome
Objects from the same launch · 6
- COSMOS 1509 DEB14535DebrisDecayed
- COSMOS 1509 DEB14536DebrisDecayed
- COSMOS 1509 DEB14539DebrisDecayed
- COSMOS 1509 DEB14540DebrisDecayed
- COSMOS 1509 DEB14541DebrisDecayed
- COSMOS 150914490PayloadDecayed
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
- 14498
- COSPAR / international designator
- 1983-112B
- SatelliteIndex id
- sat_01M28X3JNC4WAENAK62RX01C4E
- Canonical slug
- sl-4-r-b-14498
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.