Rocket body · NORAD 44826 · COSPAR 2019-084C
ELECTRON R/B
- Operator United States
- Constellation —
- Country United States
Altitude now
—
object decayed
Velocity
—
Inclination
96.98°
Period
87.6 min
87.6 min
Perigee
143km
Apogee
170km
orbit unavailableNo orbital element set on file — decayed 18 Dec 2019.· Metadata updated 9 h ago
Live position
Live position
Live position unavailable — this object re-entered the atmosphere on 18 Dec 2019 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
- ELECTRON R/BCelestrak Satcat
Ownership
Operator & country
- Operator
- —
- SATCAT owner code
- US · United States
- Country
- United States US
Launch
Launch
- Launch date
- 06 Dec 2019
- COSPAR launch id
- 2019-084
- Launch site
- Rocket Lab Launch Complex 1, Mahia
Objects from the same launch · 8
- ALE-244824PayloadDecayed
- NOOR 1A (UNICORN-2B)44827PayloadDecayed
- NOOR 1B (UNICORN-2C)44828PayloadDecayed
- FOSSASAT-144829PayloadDecayed
- ATL-144830PayloadDecayed
- SMOG-P44832PayloadDecayed
- ELECTRON KICK STAGE R/B44825Rocket bodyDecayed
- OBJECT H44831UnknownDecayed
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
Transparency
Sources & provenance
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
No events detected for this object yet. Launches, decays and orbit changes are generated by the derived-analytics connector.
Reference
Identifiers
- NORAD catalogue number
- 44826
- COSPAR / international designator
- 2019-084C
- SatelliteIndex id
- sat_01M28X3JV78GQWBWXMF7PW02AP
- Canonical slug
- electron-r-b-44826
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.