Rocket body · NORAD 832 · COSPAR 1964-038D
SL-3 R/B
- Operator Commonwealth of Independent States (former USSR)
- Constellation —
- Country Russia
Altitude now
—
object decayed
Velocity
—
Inclination
65.84°
Period
20.9 h
1,254.9 min
Perigee
100km
Apogee
64,221km
orbit unavailableNo orbital element set on file — decayed 24 Aug 1983.· Metadata updated 10 h ago
Live position
Live position
Live position unavailable — this object re-entered the atmosphere on 24 Aug 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
- 30.4 m²
CelesTrak groups
Not listed in any CelesTrak group.
Aliases
- SL-3 R/BCelestrak Satcat
Ownership
Operator & country
- Operator
- —
- SATCAT owner code
- CIS · Commonwealth of Independent States (former USSR)
- Country
- Russia RU
Launch
Launch
- Launch date
- 10 Jul 1964
- COSPAR launch id
- 1964-038
- Launch site
- Baikonur Cosmodrome (Tyuratam)
Objects from the same launch · 6
- ELEKTRON 3 DEB831DebrisInactive
- ELEKTRON 3 DEB5892DebrisDecayed
- ELEKTRON 3 DEB5893DebrisDecayed
- ELEKTRON 3 DEB29008DebrisInactive
- ELEKTRON 3829PayloadUnknown
- ELEKTRON 4830PayloadDecayed
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
- 832
- COSPAR / international designator
- 1964-038D
- SatelliteIndex id
- sat_01M28X3JJCP6W1J01F09Z6JYHD
- Canonical slug
- sl-3-r-b-832
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.