Rocket body · NORAD 52323 · COSPAR 2022-043D
CZ-2C R/B
- Operator People's Republic of China
- Constellation —
- Country China
Altitude now
—
object decayed
Velocity
—
Inclination
97.51°
Period
87.4 min
87.4 min
Perigee
131km
Apogee
157km
orbit unavailableNo orbital element set on file — decayed 20 Jun 2023.· Metadata updated 16 h ago
Live position
Live position
Live position unavailable — this object re-entered the atmosphere on 20 Jun 2023 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 Apr 2022
- COSPAR launch id
- 2022-043
- Launch site
- Jiuquan Satellite Launch Center
Objects from the same launch · 8
- CZ-2C DEB52321DebrisDecayed
- CZ-2C DEB52324DebrisDecayed
- CZ-2C DEB52325DebrisDecayed
- CZ-2C DEB52326DebrisDecayed
- CZ-2C DEB52327DebrisDecayed
- CZ-2C DEB52328DebrisDecayed
- SUPERVIEW NEO-1 0152320PayloadActive
- SUPERVIEW NEO-1 0252322PayloadActive
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
- 52323
- COSPAR / international designator
- 2022-043D
- SatelliteIndex id
- sat_01M28X3JW64PEB85AFEEFZR2RY
- Canonical slug
- cz-2c-r-b-52323
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.