Satellite · NORAD 22108 · COSPAR 1992-058A
NAVSTAR 27 (USA 84)
- Operator United States Space Force
- Constellation GPS (NAVSTAR)
- Country United States
Altitude now
—
no element set
Velocity
—
Inclination
54.67°
Period
12.8 h
767.8 min
Perigee
21,345km
Apogee
21,447km
orbit unavailableNo orbital element set on file.· Metadata updated 2 d 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
- Navigation
- Object type
- Payload
- SATCAT ops status
- Non-operational [-]
- Radar cross-section
- 2.9 m²
- Constellation membership derived
- GPS (NAVSTAR) via name_pattern
CelesTrak groups
Not listed in any CelesTrak group.
Aliases
- NAVSTAR 27 (USA 84)Celestrak Satcat
Ownership
Operator & country
- Operator
- United States Space Force
- SATCAT owner code
- US · United States
- Country
- United States US
Launch
Launch
- Launch date
- 09 Sept 1992
- COSPAR launch id
- 1992-058
Objects from the same launch · 4
- DELTA 2 DEB23300DebrisDecayed
- DELTA 2 DEB26851DebrisInactive
- DELTA 2 R/B(1)22109Rocket bodyInactive
- DELTA 2 R/B(2) [PAM-D]22110Rocket 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
- 22108
- COSPAR / international designator
- 1992-058A
- SatelliteIndex id
- sat_01M28X3JPPGDWGZYXWCDCKVJW4
- Canonical slug
- navstar-27-usa-84-22108
Orbit class, mission type and constellation membership are derived by SatelliteIndex (Navigation) — see the methodology. Positions are propagated estimates, not tracking measurements; never use them for conjunction assessment.