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HELLAS-SAT 1 (DFS 3)

NORAD 22175 Payload GEO 1992-066A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35934 km
Apogee
35940 km
Inclination
14.2°
Period
1443.8 min
Mean Motion
0.99736763 rev/day
TLE Epoch
2026-06-18 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,937 km
Orbital Velocity11,050 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0001
Semi-Major Axis42,308 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
GREC
Launch Date
1992-10-12
Launch Site
Cape Canaveral, Florida
Int'l Designator
1992-066A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
HELLAS-SAT 1 (DFS 3) is an active satellite operated by GREC, launched on 1992-10-12 from Cape Canaveral, Florida. With over 34 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,934 km and 35,940 km with an inclination of 14.2°. It travels at approximately 11,050 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 HELLAS-SAT 1 (DFS 3) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
HELLAS-SAT 1 (DFS 3) 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 14.2°, 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 HELLAS-SAT 1 (DFS 3)’s average altitude, there are currently 59 active payloads and 20 tracked debris or rocket body fragments. GREC operates approximately 10 active satellites in total.
❓ Frequently Asked Questions
HELLAS-SAT 1 (DFS 3) orbits at approximately 35,937 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 11,050 km/h — it just keeps pace with the ground below. With an inclination of 14.2°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
HELLAS-SAT 1 (DFS 3) is operated by GREC. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 22175. You can track HELLAS-SAT 1 (DFS 3) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
HELLAS-SAT 1 (DFS 3) was launched on 1992-10-12 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 HELLAS-SAT 1 (DFS 3) (NORAD ID 22175) 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.
HELLAS-SAT 1 (DFS 3) travels at approximately 11,050 km/h (6,866 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.