Skip to content
Home Library Satellite Directory AEHF 3 (USA 246)

AEHF 3 (USA 246)

NORAD 39256 Payload GEO 2013-050A ● Active
CONNECTING… GEO · NORAD 39256
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
35416 km
Apogee
36157 km
Inclination
5.3°
Period
1436.1 min
Mean Motion
1.00273110 rev/day
TLE Epoch
2026-06-19 06:00:00 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
Eccentricity0.0088
Semi-Major Axis42,158 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 US Air Force (United States)
Launch Date
2013-09-18
Launch Site
Cape Canaveral, Florida
Int'l Designator
2013-050A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
AEHF 3 (USA 246) is an active satellite operated by US Air Force (United States), launched on 2013-09-18 from Cape Canaveral, Florida. After 13 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 35,416 km and 36,157 km with an inclination of 5.3°. 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 3 (USA 246) 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 3 (USA 246) 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 5.3°, 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 3 (USA 246)’s average altitude, there are currently 713 active payloads and 58 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. United States operates approximately 12,339 active satellites in total, of which 146 share a similar altitude band with AEHF 3 (USA 246).
❓ Frequently Asked Questions
AEHF 3 (USA 246) 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 5.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
AEHF 3 (USA 246) is operated by US Air Force (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 39256. You can track AEHF 3 (USA 246) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
AEHF 3 (USA 246) was launched on 2013-09-18 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 3 (USA 246) (NORAD ID 39256) 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 3 (USA 246) 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.