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USA 81

NORAD 21949 Payload LEO 1992-023A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
782 km
Apogee
786 km
Inclination
85.0°
Period
100.5 min
Mean Motion
14.32398807 rev/day
TLE Epoch
2026-06-19 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude784 km
Orbital Velocity26,870 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.32
Eccentricity0.0003
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)
📖 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 786 km with an inclination of 85.0°. It travels at approximately 26,870 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 orbits at an average altitude of 784 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of USA 81’s average altitude, there are currently 419 active payloads and 2,230 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 85.0°, USA 81 passes over latitudes between 85.0°N and 85.0°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. United States operates approximately 12,360 active satellites in total, of which 155 share a similar altitude band with USA 81.
❓ Frequently Asked Questions
USA 81 orbits in Low Earth Orbit (LEO) at altitudes between 782 km (perigee) and 786 km (apogee), with an average altitude of approximately 784 km. It completes one orbit every 101 minutes, travelling at approximately 26,870 km/h (16,696 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 or browse all operators in the operator directory.
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. View the full satellite launch log.
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. You can also browse the satellite directory to find other tracked objects.
USA 81 travels at approximately 26,870 km/h (16,696 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.