Skip to content
SatelliteIndex

Satellite · NORAD 41871 · COSPAR 2016-062C

LEMUR-2-XIAOQING

DecayedPayloadLEOEarth observation derived

Altitude now

—

object decayed

Velocity

—

Inclination

51.60°

Period

88.2 min

88.2 min

Perigee

180km

Apogee

192km

orbit unavailableNo orbital element set on file — decayed 10 Apr 2023.· Metadata updated 9 h ago

Live position

Live position

Live position unavailable — this object re-entered the atmosphere on 10 Apr 2023 and is no longer tracked.

Mission

Mission & classification

Mission type derived
Earth observation
Object type
Payload
SATCAT ops status
Decayed [D]
Radar cross-section
0.1 m²
Constellation membership derived
Spire Lemur via name_pattern

CelesTrak groups

Not listed in any CelesTrak group.

Aliases

  • LEMUR-2-XIAOQINGCelestrak Satcat

Ownership

Operator & country

Operator
Spire Global
SATCAT owner code
US · United States
Country
United States US

Launch

Launch

Launch page →
Launch date
17 Oct 2016
COSPAR launch id
2016-062
Launch site
Wallops Flight Facility / MARS, Virginia

Objects from the same launch · 5

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
41871
COSPAR / international designator
2016-062C
SatelliteIndex id
sat_01M28X3JTSXD94KEX9QRKCNENM
Canonical slug
lemur-2-xiaoqing-41871

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