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SatelliteIndex

Rocket body · NORAD 58926 · COSPAR 2024-024K

JIELONG-3 R/B

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

Altitude now

—

object decayed

Velocity

—

Inclination

97.37°

Period

87.1 min

87.1 min

Perigee

119km

Apogee

146km

orbit unavailableNo orbital element set on file — decayed 17 Mar 2024.· Metadata updated 8 h ago

Live position

Live position

Live position unavailable — this object re-entered the atmosphere on 17 Mar 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

  • 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
03 Feb 2024
COSPAR launch id
2024-024
Launch site
South China Sea Launch Area (sea launch)

Objects from the same launch · 10

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
58926
COSPAR / international designator
2024-024K
SatelliteIndex id
sat_01M28X3JWNH78KWM3PVRS2WF7J
Canonical slug
jielong-3-r-b-58926

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.