Rocket body · NORAD 69537 · COSPAR 2026-128C
ZHUQUE-2E R/B
- Operator People's Republic of China
- Constellation —
- Country China
Altitude now
—
no element set
Velocity
—
Inclination
54.52°
Period
91.6 min
91.6 min
Perigee
320km
Apogee
382km
orbit unavailableNo orbital element set on file.· Metadata updated 8 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
- —
CelesTrak groups
Not listed in any CelesTrak group.
Aliases
- ZHUQUE-2E R/BCelestrak Satcat
Ownership
Operator & country
- Operator
- —
- SATCAT owner code
- PRC · People's Republic of China
- Country
- China CN
Launch
Launch
- Launch date
- 09 Jun 2026
- COSPAR launch id
- 2026-128
- Launch site
- Jiuquan Satellite Launch Center
Objects from the same launch · 9
- ZHUQUE-2E DEB69629DebrisDecayed
- ZHUQUE-2E DEB69630DebrisInactive
- ZHUQUE-2E DEB69631DebrisDecayed
- ZHUQUE-2E DEB69632DebrisDecayed
- ZHUQUE-2E DEB69633DebrisDecayed
- ZHUQUE-2E DEB69634DebrisDecayed
- ZHUQUE-2E DEB69635DebrisDecayed
- DTC TEST OBJECT A69472PayloadActive
- DTC TEST OBJECT B69473PayloadActive
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
- 69537
- COSPAR / international designator
- 2026-128C
- SatelliteIndex id
- sat_01M28X3JX0JMPWEX8W8KDSF6T6
- Canonical slug
- zhuque-2e-r-b-69537
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.