Rocket body · NORAD 8615 · COSPAR 1976-008J
SL-8 R/B
- Operator Commonwealth of Independent States (former USSR)
- Constellation —
- Country Russia
Altitude now
—
no element set
Velocity
—
Inclination
74.05°
Period
118.0 min
118.0 min
Perigee
1,482km
Apogee
1,695km
orbit unavailableNo orbital element set on file.· Metadata updated 17 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
- 5.9 m²
CelesTrak groups
Not listed in any CelesTrak group.
Aliases
- SL-8 R/BCelestrak Satcat
Ownership
Operator & country
- Operator
- —
- SATCAT owner code
- CIS · Commonwealth of Independent States (former USSR)
- Country
- Russia RU
Launch
Launch
- Launch date
- 28 Jan 1976
- COSPAR launch id
- 1976-008
- Launch site
- Plesetsk Cosmodrome
Objects from the same launch · 8
- COSMOS 7918607PayloadUnknown
- COSMOS 7928608PayloadUnknown
- COSMOS 7938609PayloadUnknown
- COSMOS 7948610PayloadUnknown
- COSMOS 7958611PayloadUnknown
- COSMOS 7968612PayloadUnknown
- COSMOS 7978613PayloadUnknown
- COSMOS 7988614PayloadUnknown
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
- 8615
- COSPAR / international designator
- 1976-008J
- SatelliteIndex id
- sat_01M28X3JMBK9PSYR3G806J1WFK
- Canonical slug
- sl-8-r-b-8615
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.