Rocket body · NORAD 19122 · COSPAR 1988-040B
ARIANE 2 R/B
- Operator France
- Constellation —
- Country France
Altitude now
—
no element set
Velocity
—
Inclination
7.31°
Period
10.1 h
604.4 min
Perigee
486km
Apogee
34,114km
orbit unavailableNo orbital element set on file.· Metadata updated 21 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
- 1.2 m²
CelesTrak groups
Not listed in any CelesTrak group.
Aliases
- ARIANE 2 R/BCelestrak Satcat
Ownership
Operator & country
- Operator
- —
- SATCAT owner code
- FR · France
- Country
- France FR
Launch
Launch
- Launch date
- 17 May 1988
- COSPAR launch id
- 1988-040
- Launch site
- Guiana Space Centre, Kourou
Objects from the same launch · 8
- ARIANE 2 DEB27593DebrisInactive
- ARIANE 2 DEB27594DebrisInactive
- ARIANE 2 DEB27595DebrisInactive
- ARIANE 2 DEB28562DebrisInactive
- ARIANE 2 DEB33533DebrisInactive
- ARIANE 2 DEB33534DebrisInactive
- ARIANE 2 DEB33535DebrisInactive
- NSS-513 (INTELSAT 513)19121PayloadUnknown
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
- 19122
- COSPAR / international designator
- 1988-040B
- SatelliteIndex id
- sat_01M28X3JP5YR60YP1V514XEW2Z
- Canonical slug
- ariane-2-r-b-19122
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.