Skip to content
SatelliteIndex

Rocket body · NORAD 40978 · COSPAR 2015-058Q

ATLAS 5 CENTAUR R/B

InactiveRocket bodyLEORocket body derived

Altitude now

—

no element set

Velocity

—

Inclination

64.77°

Period

95.6 min

95.6 min

Perigee

467km

Apogee

629km

orbit unavailableNo orbital element set on file.· Metadata updated 11 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
—

CelesTrak groups

Not listed in any CelesTrak group.

Aliases

  • ATLAS 5 CENTAUR R/BCelestrak Satcat

Ownership

Operator & country

Operator
—
SATCAT owner code
US · United States
Country
United States US

Launch

Launch

Launch page →
Launch date
08 Oct 2015
COSPAR launch id
2015-058
Launch site
Vandenberg Space Force Base (Western Range), California

Objects from the same launch · 15

All objects from launch 2015-058 →

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
40978
COSPAR / international designator
2015-058Q
SatelliteIndex id
sat_01M28X3JTN11DX2DFQVEERGAH5
Canonical slug
atlas-5-centaur-r-b-40978

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.