Skip to content
Home › Library › Satellite Directory › ATS 6

ATS 6

NORAD 7318 Payload GEO 1974-039A ● Active
CONNECTING… GEO · NORAD 7318
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
35170 km
Apogee
35459 km
Inclination
1.7°
Period
1412.0 min
Mean Motion
1.01979586 rev/day
TLE Epoch
2026-10-21 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,315 km
Orbital Velocity11,132 km/h
Velocity3.09 km/s
Orbital Period23 hours 32 minutes
Orbits / Day1.02
Eccentricity0.0035
Semi-Major Axis41,686 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 GSFC (United States)
Launch Date
1974-05-30
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1974-039A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ATS 6 is an active satellite operated by GSFC (United States), launched on 1974-05-30 from Cape Canaveral Space Force Station, United States on the ATS F launch. After more than 52 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Geostationary Orbit (GEO) at altitudes between 35,170 km and 35,459 km with an inclination of 1.7°. It travels at approximately 11,132 km/h (3.09 km/s), completing one full orbit every 23 hours 32 minutes — that’s roughly 1.02 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 ATS 6 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ATS 6 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 1.7°, 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 ATS 6’s average altitude, there are currently 3 active payloads and 10 tracked debris or rocket body fragments. United States operates approximately 13,279 active satellites in total, of which 3 share a similar altitude band with ATS 6.
❓ Frequently Asked Questions
ATS 6 orbits at approximately 35,315 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 11,132 km/h — it just keeps pace with the ground below. With an inclination of 1.7°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
ATS 6 is operated by GSFC (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 7318. You can track ATS 6 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ATS 6 was launched on 1974-05-30 from Cape Canaveral Space Force Station, United States, 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 ATS 6 (NORAD ID 7318) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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.
ATS 6 travels at approximately 11,132 km/h (6,917 mph) — roughly 3.09 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.