Rocket body · NORAD 43916 · COSPAR 2018-112H
CZ-2D R/B
- Operator People's Republic of China
- Constellation —
- Country China
Altitude now
—
object decayed
Velocity
—
Inclination
50.04°
Period
87.3 min
87.3 min
Perigee
141km
Apogee
143km
orbit unavailableNo orbital element set on file — decayed 01 Jan 2019.· Metadata updated 12 h ago
Live position
Live position
Live position unavailable — this object re-entered the atmosphere on 01 Jan 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-2D R/BCelestrak Satcat
Ownership
Operator & country
- Operator
- —
- SATCAT owner code
- PRC · People's Republic of China
- Country
- China CN
Launch
Launch
- Launch date
- 29 Dec 2018
- COSPAR launch id
- 2018-112
- Launch site
- Jiuquan Satellite Launch Center
Objects from the same launch · 7
- YUNHAI-2 01A43909PayloadActive
- YUNHAI-2 01B43910PayloadActive
- YUNHAI-2 01C43911PayloadActive
- YUNHAI-2 01D43912PayloadActive
- YUNHAI-2 01E43913PayloadActive
- HONGYAN 1 (CHONGQING)43914PayloadActive
- YUNHAI-2 01F43915PayloadActive
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
- 43916
- COSPAR / international designator
- 2018-112H
- SatelliteIndex id
- sat_01M28X3JV2P2MKKM71AC7EK21E
- Canonical slug
- cz-2d-r-b-43916
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.