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SatelliteIndex

Satellite · NORAD 46904 · COSPAR 2020-080A

TIANQI-11

DecayedPayloadLEOIoT / M2M derived

Altitude now

—

object decayed

Velocity

—

Inclination

97.48°

Period

88.4 min

88.4 min

Perigee

191km

Apogee

203km

orbit unavailableNo orbital element set on file — decayed 05 Nov 2023.· Metadata updated 9 h ago

Live position

Live position

Live position unavailable — this object re-entered the atmosphere on 05 Nov 2023 and is no longer tracked.

Mission

Mission & classification

Mission type derived
IoT / M2M
Object type
Payload
SATCAT ops status
Decayed [D]
Radar cross-section
—
Constellation membership derived
Tianqi via name_pattern

CelesTrak groups

Not listed in any CelesTrak group.

Aliases

  • TIANQI-11Celestrak Satcat

Ownership

Operator & country

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

Launch

Launch

Launch page →
Launch date
07 Nov 2020
COSPAR launch id
2020-080
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
46904
COSPAR / international designator
2020-080A
SatelliteIndex id
sat_01M28X3JVG4WHVV4JEHFZ61X3W
Canonical slug
tianqi-11-46904

Orbit class, mission type and constellation membership are derived by SatelliteIndex (IoT / M2M) — see the methodology. Positions are propagated estimates, not tracking measurements; never use them for conjunction assessment.