Rocket body · NORAD 43667 · COSPAR 2018-083F
CZ-2C R/B
- Operator People's Republic of China
- Constellation —
- Country China
Altitude now
—
object decayed
Velocity
—
Inclination
97.58°
Period
87.2 min
87.2 min
Perigee
130km
Apogee
141km
orbit unavailableNo orbital element set on file — decayed 05 Feb 2019.· Metadata updated 9 h ago
Live position
Live position
Live position unavailable — this object re-entered the atmosphere on 05 Feb 2019 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
- CZ-2C R/BCelestrak Satcat
Ownership
Operator & country
- Operator
- —
- SATCAT owner code
- PRC · People's Republic of China
- Country
- China CN
Launch
Launch
- Launch date
- 29 Oct 2018
- COSPAR launch id
- 2018-083
- Launch site
- Jiuquan Satellite Launch Center
Objects from the same launch · 7
- CFOSAT43662PayloadActive
- CUBEBEL-1 (BSUSAT-1)43666PayloadDecayed
- CHANGSHAGAOXIN (TY 4-01)43669PayloadDecayed
- OBJECT B43663UnknownDecayed
- OBJECT C43664UnknownDecayed
- OBJECT D43665UnknownDecayed
- OBJECT G43668UnknownDecayed
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
- 43667
- COSPAR / international designator
- 2018-083F
- SatelliteIndex id
- sat_01M28X3JV2P2MKKM71AC7EK1VY
- Canonical slug
- cz-2c-r-b-43667
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.