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SatelliteIndex

Rocket body · NORAD 41624 · COSPAR 2016-042A

YZ-1A R/B

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

Altitude now

—

object decayed

Velocity

—

Inclination

40.81°

Period

91.2 min

91.2 min

Perigee

288km

Apogee

382km

orbit unavailableNo orbital element set on file — decayed 27 Jun 2016.· Metadata updated 19 h ago

Live position

Live position

Live position unavailable — this object re-entered the atmosphere on 27 Jun 2016 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
11.9 m²

CelesTrak groups

Not listed in any CelesTrak group.

Aliases

  • YZ-1A 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
25 Jun 2016
COSPAR launch id
2016-042
Launch site
Wenchang Space Launch Site, Hainan

Objects from the same launch · 12

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
41624
COSPAR / international designator
2016-042A
SatelliteIndex id
sat_01M28X3JTR27RWATBPVQ3JHQRP
Canonical slug
yz-1a-r-b-41624

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.