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SatelliteIndex

Rocket body · NORAD 58507 · COSPAR 2023-190C

JIELONG-3 R/B

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

Altitude now

—

no element set

Velocity

—

Inclination

86.56°

Period

94.3 min

94.3 min

Perigee

335km

Apogee

639km

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

  • JIELONG-3 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
05 Dec 2023
COSPAR launch id
2023-190
Launch site
South China Sea Launch Area (sea launch)

Objects from the same launch · 2

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
58507
COSPAR / international designator
2023-190C
SatelliteIndex id
sat_01M28X3JWNH78KWM3PVRS2WF40
Canonical slug
jielong-3-r-b-58507

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.