AEHF 2 (USA 235)
NORAD 38254
Payload
GEO
2012-019A
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GEO · NORAD 38254
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
35777 km
Apogee
35796 km
Inclination
6.7°
Period
1436.1 min
Mean Motion
1.00271640 rev/day
TLE Epoch
2026-06-19 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,787 km
Orbital Velocity11,070 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0002
Semi-Major Axis42,158 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 US Air Force (United States)
Launch Date
2012-05-04
Launch Site
Cape Canaveral, Florida
Int'l Designator
2012-019A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
AEHF 2 (USA 235) is an active satellite operated by US Air Force (United States), launched on 2012-05-04 from Cape Canaveral, Florida. After 14 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 35,777 km and 35,796 km with an inclination of 6.7°. It travels at approximately 11,070 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks AEHF 2 (USA 235) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
AEHF 2 (USA 235) occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 6.7°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of AEHF 2 (USA 235)’s average altitude, there are currently 713 active payloads and 59 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. United States operates approximately 12,360 active satellites in total, of which 146 share a similar altitude band with AEHF 2 (USA 235).
❓ Frequently Asked Questions
AEHF 2 (USA 235) orbits at approximately 35,787 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,070 km/h — it just keeps pace with the ground below. With an inclination of 6.7°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
AEHF 2 (USA 235) is operated by US Air Force (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 38254. You can track AEHF 2 (USA 235) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
AEHF 2 (USA 235) was launched on 2012-05-04 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. View the full satellite launch log.
Yes — Orbital Radar tracks AEHF 2 (USA 235) (NORAD ID 38254) 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.
AEHF 2 (USA 235) travels at approximately 11,070 km/h (6,878 mph) — roughly 3.07 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.