Rocket body · NORAD 7219 · COSPAR 1974-015B
THOR BURNER 2A R/B
- Operator United States
- Constellation —
- Country United States
Altitude now
—
no element set
Velocity
—
Inclination
99.08°
Period
101.0 min
101.0 min
Perigee
758km
Apogee
851km
orbit unavailableNo orbital element set on file.· Metadata updated 13 h ago
Live position
Live position
Live position unavailable — no public orbital element set exists for this object (it may be classified, untracked or too small to catalogue).
Mission
Mission & classification
- Mission type derived
- Rocket body
- Object type
- Rocket body
- Radar cross-section
- 1.1 m²
CelesTrak groups
Not listed in any CelesTrak group.
Aliases
- THOR BURNER 2A R/BCelestrak Satcat
Ownership
Operator & country
- Operator
- —
- SATCAT owner code
- US · United States
- Country
- United States US
Launch
Launch
- Launch date
- 16 Mar 1974
- COSPAR launch id
- 1974-015
Objects from the same launch · 7
- THOR BURNER 2A DEB28591DebrisInactive
- THOR BURNER 2A DEB28592DebrisDecayed
- THOR BURNER 2A DEB28593DebrisInactive
- THOR BURNER 2A DEB29139DebrisInactive
- THOR BURNER 2A DEB36296DebrisDecayed
- THOR BURNER 2A DEB37584DebrisInactive
- OPS 8579 (DMSP 5B F5)7218PayloadUnknown
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
- 7219
- COSPAR / international designator
- 1974-015B
- SatelliteIndex id
- sat_01M28X3JKHTEGKNM7BJD9B6NJ7
- Canonical slug
- thor-burner-2a-r-b-7219
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.