Rocket body · NORAD 2825 · COSPAR 1967-053B
THOR AGENA D R/B
- Operator United States
- Constellation —
- Country United States
Altitude now
—
no element set
Velocity
—
Inclination
69.97°
Period
103.0 min
103.0 min
Perigee
898km
Apogee
905km
orbit unavailableNo orbital element set on file.· Metadata updated 12 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
- 4.6 m²
CelesTrak groups
Not listed in any CelesTrak group.
Aliases
- THOR AGENA D R/BCelestrak Satcat
Ownership
Operator & country
- Operator
- —
- SATCAT owner code
- US · United States
- Country
- United States US
Launch
Launch
- Launch date
- 31 May 1967
- COSPAR launch id
- 1967-053
Objects from the same launch · 10
- P/L 153 DEB19245DebrisInactive
- P/L 153 DEB39247DebrisDecayed
- OPS 5712 (P/L 160)2826PayloadActive
- GGSE 42828PayloadUnknown
- GGSE 52834PayloadUnknown
- TIMATION 12847PayloadUnknown
- SURCAL 1592872PayloadActive
- OPS 5712 (P/L 152)2873PayloadUnknown
- OPS 5712 (P/L 153)2874PayloadActive
- SURCAL 150B2909PayloadDecayed
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
- 2825
- COSPAR / international designator
- 1967-053B
- SatelliteIndex id
- sat_01M28X3JJR8VVZXS40YM3E3E1Y
- Canonical slug
- thor-agena-d-r-b-2825
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.