Rocket body · NORAD 29233 · COSPAR 2006-022D
SL-12 R/B(2)
- Operator Commonwealth of Independent States (former USSR)
- Constellation —
- Country Russia
Altitude now
—
no element set
Velocity
—
Inclination
12.61°
Period
23.8 h
1,425.6 min
Perigee
35,368km
Apogee
35,794km
orbit unavailableNo orbital element set on file.· Metadata updated 10 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
- 4.0 m²
CelesTrak groups
Not listed in any CelesTrak group.
Aliases
- SL-12 R/B(2)Celestrak Satcat
Ownership
Operator & country
- Operator
- —
- SATCAT owner code
- CIS · Commonwealth of Independent States (former USSR)
- Country
- Russia RU
Launch
Launch
- Launch date
- 17 Jun 2006
- COSPAR launch id
- 2006-022
- Launch site
- Baikonur Cosmodrome (Tyuratam)
Objects from the same launch · 7
- SL-12 PLAT29231DebrisDecayed
- SL-12 DEB29234DebrisDecayed
- SL-12 DEB29235DebrisDecayed
- SL-12 DEB29238DebrisDecayed
- SL-12 DEB29239DebrisDecayed
- KAZSAT-129230PayloadUnknown
- SL-12 R/B(1)29232Rocket 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
- 29233
- COSPAR / international designator
- 2006-022D
- SatelliteIndex id
- sat_01M28X3JQXR6FFEMCFY4ZEC0BE
- Canonical slug
- sl-12-r-b-2-29233
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.