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USA 81

NORAD 21949 Payload LEO 1992-023A ● Active
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
782 km
Apogee
785 km
Inclination
85.0°
Period
100.5 min
Mean Motion
14.32370485 rev/day
TLE Epoch
2026-03-17 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude784 km
Orbital Velocity26,871 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.32
Eccentricity0.0002
Semi-Major Axis7,155 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1992-04-25
Launch Site
Vandenberg SFB, California
Int'l Designator
1992-023A
Object Type
Payload
RCS Size
Large (>1 m²)
🔗 Constellation / Groups
visual
📖 About This Object
USA 81 is an active satellite operated by United States, launched on 1992-04-25 from Vandenberg SFB, California. With over 34 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 782 km and 785 km with an inclination of 85.0°. It travels at approximately 26,871 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.32 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Orbital Radar tracks USA 81 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
USA 81 occupies the mid-LEO band between 600 and 1,000 km, where atmospheric drag is minimal but radiation exposure remains low. This altitude range balances orbital longevity (decades to centuries) with reasonable ground coverage, making it popular for remote sensing constellations, scientific instruments and weather satellites. Debris concerns are significant here because objects persist far longer than in lower orbits.
❓ Frequently Asked Questions
USA 81 orbits in Low Earth Orbit (LEO) at altitudes between 782 km (perigee) and 785 km (apogee), with an average altitude of approximately 784 km. It completes one orbit every 101 minutes, travelling at approximately 26,871 km/h (16,697 mph).
USA 81 is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 21949. You can track USA 81 in real time on Orbital Radar’s live tracker.
USA 81 was launched on 1992-04-25 from Vandenberg SFB, California, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years.
Yes — Orbital Radar tracks USA 81 (NORAD ID 21949) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time.
USA 81 travels at approximately 26,871 km/h (16,697 mph) — roughly 7.46 km/s. It completes 14.32 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.