Rocket body · NORAD 11147 · COSPAR 1978-113D
TITAN 3C TRANSTAGE R/B
- Operator United States
- Constellation —
- Country United States
Altitude now
—
no element set
Velocity
—
Inclination
10.57°
Period
1.1 d
1,535.9 min
Perigee
36,598km
Apogee
38,839km
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
- 3.1 m²
CelesTrak groups
Not listed in any CelesTrak group.
Aliases
- TITAN 3C TRANSTAGE R/BCelestrak Satcat
Ownership
Operator & country
- Operator
- —
- SATCAT owner code
- US · United States
- Country
- United States US
Launch
Launch
- Launch date
- 14 Dec 1978
- COSPAR launch id
- 1978-113
Objects from the same launch · 7
- OPS 9442 (DSCS 2-12) DEB59989DebrisInactive
- OPS 9442 (DSCS 2-12) DEB59990DebrisInactive
- OPS 9442 (DSCS 2-12) DEB59991DebrisInactive
- OPS 9442 (DSCS 2-12) DEB59992DebrisInactive
- OPS 9441 (DSCS 2-11)11144PayloadUnknown
- OPS 9442 (DSCS 2-12)11145PayloadUnknown
- TITAN 3C R/B(1)11146Rocket bodyDecayed
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
- 11147
- COSPAR / international designator
- 1978-113D
- SatelliteIndex id
- sat_01M28X3JMSWGAB1RH93X50S2QN
- Canonical slug
- titan-3c-transtage-r-b-11147
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.