Rocket body · NORAD 39211 · COSPAR 2013-037D
CZ-4C R/B
- Operator People's Republic of China
- Constellation —
- Country China
Altitude now
—
no element set
Velocity
—
Inclination
97.96°
Period
93.5 min
93.5 min
Perigee
405km
Apogee
488km
orbit unavailableNo orbital element set on file.· Metadata updated 10 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
- 6.5 m²
CelesTrak groups
Not listed in any CelesTrak group.
Aliases
- CZ-4C R/BCelestrak Satcat
Ownership
Operator & country
- Operator
- —
- SATCAT owner code
- PRC · People's Republic of China
- Country
- China CN
Launch
Launch
- Launch date
- 19 Jul 2013
- COSPAR launch id
- 2013-037
- Launch site
- Taiyuan Satellite Launch Center
Objects from the same launch · 8
- CZ-4C DEB39212DebrisInactive
- CZ-4C DEB39213DebrisInactive
- CZ-4C DEB39214DebrisInactive
- CZ-4C DEB39231DebrisInactive
- SHIYAN-7 DEB39357DebrisInactive
- SHIYAN-7 (SY-7)39208PayloadActive
- CHUANGXIN-3 (CX-3)39209PayloadActive
- SHIJIAN-15 (SJ-15)39210PayloadActive
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
- 39211
- COSPAR / international designator
- 2013-037D
- SatelliteIndex id
- sat_01M28X3JTCFZ3P0VSPHHKZ2K00
- Canonical slug
- cz-4c-r-b-39211
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.