ASTRA 2C
NORAD 26853
Payload
GEO
2001-025A
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GEO · NORAD 26853
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Altitude (km)
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🛰️ Orbital Parameters
Perigee
36113 km
Apogee
36159 km
Inclination
8.2°
Period
1454.0 min
Mean Motion
0.99038050 rev/day
TLE Epoch
2026-06-19 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,136 km
Orbital Velocity11,024 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0005
Semi-Major Axis42,507 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
SES S.A. (SES)
Launch Date
2001-06-16
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2001-025A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ASTRA 2C is an active satellite operated by SES S.A. (SES), launched on 2001-06-16 from Baikonur, Kazakhstan. With over 25 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,113 km and 36,159 km with an inclination of 8.2°. It travels at approximately 11,024 km/h (3.06 km/s), completing one full orbit every 24.2 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 2C 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 2C 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 8.2°, 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 ASTRA 2C’s average altitude, there are currently 184 active payloads and 7 tracked debris or rocket body fragments. SES operates approximately 77 active satellites in total, of which 21 share a similar altitude band with ASTRA 2C.
🔗 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 2C orbits at approximately 36,136 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 11,024 km/h — it just keeps pace with the ground below. With an inclination of 8.2°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
ASTRA 2C is operated by SES S.A. (SES). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 26853. You can track ASTRA 2C in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ASTRA 2C was launched on 2001-06-16 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. View the full satellite launch log.
Yes — Orbital Radar tracks ASTRA 2C (NORAD ID 26853) 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.
ASTRA 2C travels at approximately 11,024 km/h (6,850 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.