Rocket body · NORAD 37932 · COSPAR 2011-068C
CZ-2D R/B
- Operator People's Republic of China
- Constellation —
- Country China
Altitude now
—
no element set
Velocity
—
Inclination
98.90°
Period
101.2 min
101.2 min
Perigee
789km
Apogee
842km
orbit unavailableNo orbital element set on file.· Metadata updated 9 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
- 11.1 m²
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
- 20 Nov 2011
- COSPAR launch id
- 2011-068
- Launch site
- Jiuquan Satellite Launch Center
Objects from the same launch · 8
- CZ-2D DEB38176DebrisInactive
- CZ-2D DEB38177DebrisInactive
- CZ-2D DEB38178DebrisInactive
- CZ-2D DEB38179DebrisInactive
- CZ-2D DEB38180DebrisInactive
- CZ-2D DEB38327DebrisInactive
- CHUANGXIN 1-03 (CX-1-03)37930PayloadActive
- SHIYAN-4 (SY-4)37931PayloadActive
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
- 37932
- COSPAR / international designator
- 2011-068C
- SatelliteIndex id
- sat_01M28X3JSE362D8XD7RQ8Y23KN
- Canonical slug
- cz-2d-r-b-37932
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.