Rocket body · NORAD 38712 · COSPAR 2012-039F
FREGAT R/B
- Operator Commonwealth of Independent States (former USSR)
- Constellation —
- Country Russia
Altitude now
—
object decayed
Velocity
—
Inclination
98.95°
Period
93.1 min
93.1 min
Perigee
40km
Apogee
810km
orbit unavailableNo orbital element set on file — decayed 22 Jul 2012.· Metadata updated 9 h ago
Live position
Live position
Live position unavailable — this object re-entered the atmosphere on 22 Jul 2012 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
- FREGAT R/BCelestrak Satcat
Ownership
Operator & country
- Operator
- —
- SATCAT owner code
- CIS · Commonwealth of Independent States (former USSR)
- Country
- Russia RU
Launch
Launch
- Launch date
- 22 Jul 2012
- COSPAR launch id
- 2012-039
- Launch site
- Baikonur Cosmodrome (Tyuratam)
Objects from the same launch · 7
- TET-1 DEB44597DebrisDecayed
- KANOPUS-V 138707PayloadDecayed
- BKA 238708PayloadDecayed
- EXACTVIEW-1 (ADS-1B)38709PayloadActive
- TET-138710PayloadDecayed
- MKA-PN 138711PayloadActive
- SL-26 R/B38713Rocket bodyDecayed
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
- 38712
- COSPAR / international designator
- 2012-039F
- SatelliteIndex id
- sat_01M28X3JTAW1JSQXQGJB0BJE1J
- Canonical slug
- fregat-r-b-38712
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.