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SatelliteIndex

Satellite · NORAD 56976 · COSPAR 2023-084AW

SPACEBEE-174

DecayedPayloadLEOIoT / M2M derived

Altitude now

—

object decayed

Velocity

—

Inclination

97.52°

Period

87.5 min

87.5 min

Perigee

146km

Apogee

159km

orbit unavailableNo orbital element set on file — decayed 08 Nov 2024.· Metadata updated 8 h ago

Live position

Live position

Live position unavailable — this object re-entered the atmosphere on 08 Nov 2024 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
Swarm (SpaceBEE) via name_pattern

CelesTrak groups

Not listed in any CelesTrak group.

Aliases

  • SPACEBEE-174Celestrak Satcat

Ownership

Operator & country

Operator
Swarm Technologies (SpaceX)
SATCAT owner code
US · United States
Country
United States US

Launch

Launch

Launch page →
Launch date
12 Jun 2023
COSPAR launch id
2023-084
Launch site
Vandenberg Space Force Base (Western Range), California

Objects from the same launch · 40+

All objects from launch 2023-084 →

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
56976
COSPAR / international designator
2023-084AW
SatelliteIndex id
sat_01M28X3JWJ4V73ZBXBB7G65N4A
Canonical slug
spacebee-174-56976

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.