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SatelliteIndex

Rocket body · NORAD 57319 · COSPAR 2023-097A

ZHUQUE-2 R/B

DecayedRocket bodyLEORocket body derived
  • Operator People's Republic of China
  • Constellation —
  • Country China

Altitude now

—

object decayed

Velocity

—

Inclination

97.18°

Period

87.1 min

87.1 min

Perigee

126km

Apogee

137km

orbit unavailableNo orbital element set on file — decayed 29 Nov 2024.· Metadata updated 26 h ago

Live position

Live position

Live position unavailable — this object re-entered the atmosphere on 29 Nov 2024 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

  • ZHUQUE-2 R/BCelestrak Satcat

Ownership

Operator & country

Operator
—
SATCAT owner code
PRC · People's Republic of China
Country
China CN

Launch

Launch

Launch page →
Launch date
12 Jul 2023
COSPAR launch id
2023-097
Launch site
Jiuquan Satellite Launch Center

Objects from the same launch

No other catalogued object is linked to this launch.

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

UN Register of Objects Launched into Outer Space (UNOOSA) — connector planned, not yet ingested; registration unavailable

Transparency

Sources & provenance

All sources →

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

All 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
57319
COSPAR / international designator
2023-097A
SatelliteIndex id
sat_01M28X3JWKEFHXNNBKVGP9N8BE
Canonical slug
zhuque-2-r-b-57319

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.