ASTRA 1C
NORAD 22653
Payload
GEO
1993-031A
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GEO · NORAD 22653
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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
36169 km
Apogee
36216 km
Inclination
12.8°
Period
1456.9 min
Mean Motion
0.98840905 rev/day
TLE Epoch
2026-05-08 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,193 km
Orbital Velocity11,017 km/h
Velocity3.06 km/s
Orbital Period24.3 hours
Orbits / Day0.99
Eccentricity0.0006
Semi-Major Axis42,564 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
SES
Launch Date
1993-05-12
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1993-031A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ASTRA 1C is an active satellite operated by SES, launched on 1993-05-12 from Guiana Space Centre, Kourou. With over 33 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,169 km and 36,216 km with an inclination of 12.8°. It travels at approximately 11,017 km/h (3.06 km/s), completing one full orbit every 24.3 hours — that’s roughly 0.99 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 ASTRA 1C in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ASTRA 1C occupies geostationary orbit (GEO) at approximately 35,786 km above the equator. At this precise altitude, the satellite’s orbital period matches the Earth’s rotation — so it appears to hover over a fixed point on the equator. GEO is used primarily for broadcast television, weather monitoring (Meteosat, GOES) and wideband communications. Only about 560 active satellites occupy the GEO belt, but its commercial value is immense: a single GEO slot can cover roughly one-third of the Earth’s surface. This satellite has a non-zero inclination of 12.8°, meaning it traces a small figure-of-eight pattern relative to the ground rather than remaining perfectly stationary. This can indicate an aging satellite whose stationkeeping fuel is running low, or a deliberate inclined-orbit strategy to extend operational life.
🔗 SES Fleet
This satellite is operated by SES, a major global satellite operator headquartered in Luxembourg. SES operates a multi-orbit fleet including GEO satellites for video broadcasting and enterprise connectivity, and the O3b/O3b mPOWER MEO constellation for high-throughput, low-latency data services.
❓ Frequently Asked Questions
ASTRA 1C orbits at approximately 36,193 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 11,017 km/h — it just keeps pace with the ground below. With an inclination of 12.8°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed.
ASTRA 1C is operated by SES. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 22653. You can track ASTRA 1C in real time on Orbital Radar’s live tracker.
ASTRA 1C was launched on 1993-05-12 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions.
Yes — Orbital Radar tracks ASTRA 1C (NORAD ID 22653) 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.
ASTRA 1C travels at approximately 11,017 km/h (6,845 mph) — roughly 3.06 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.