Skip to content
SatelliteIndex

Rocket body · NORAD 21141 · COSPAR 1991-015C

ARIANE 44LP R/B

DecayedRocket bodyLEORocket body derived
  • Operator France
  • Constellation —
  • Country France

Altitude now

—

object decayed

Velocity

—

Inclination

6.88°

Period

93.2 min

93.2 min

Perigee

119km

Apogee

748km

orbit unavailableNo orbital element set on file — decayed 10 Feb 2002.· Metadata updated 10 h ago

Live position

Live position

Live position unavailable — this object re-entered the atmosphere on 10 Feb 2002 and is no longer tracked.

Mission

Mission & classification

Mission type derived
Rocket body
Object type
Rocket body
SATCAT ops status
Decayed [D]
Radar cross-section
37.8 m²

CelesTrak groups

Not listed in any CelesTrak group.

Aliases

  • ARIANE 44LP R/BCelestrak Satcat

Ownership

Operator & country

Operator
—
SATCAT owner code
FR · France
Country
France FR

Launch

Launch

Launch page →
Launch date
02 Mar 1991
COSPAR launch id
1991-015
Launch site
Guiana Space Centre, Kourou

Objects from the same launch · 15

All objects from launch 1991-015 →

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

UN Register of Objects Launched into Outer Space (UNOOSA) — connector planned, not yet ingested; registration unavailable

Transparency

Sources & provenance

All sources →

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

All 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
21141
COSPAR / international designator
1991-015C
SatelliteIndex id
sat_01M28X3JPHMZEEK2X1REP5E48D
Canonical slug
ariane-44lp-r-b-21141

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.