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TURKSAT 2A

NORAD 26666 Payload GEO 2001-002A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36334 km
Apogee
36417 km
Inclination
9.0°
Period
1466.3 min
Mean Motion
0.98208594 rev/day
TLE Epoch
2026-06-19 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,376 km
Orbital Velocity10,993 km/h
Velocity3.05 km/s
Orbital Period24.4 hours
Orbits / Day0.98
Eccentricity0.0010
Semi-Major Axis42,747 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
Türksat (Turkey)
Launch Date
2001-01-10
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2001-002A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
TURKSAT 2A is an active satellite operated by Türksat (Turkey), launched on 2001-01-10 from Guiana Space Centre, Kourou. With over 25 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,334 km and 36,417 km with an inclination of 9.0°. It travels at approximately 10,993 km/h (3.05 km/s), completing one full orbit every 24.4 hours — that’s roughly 0.98 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 TURKSAT 2A in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
TURKSAT 2A 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 9.0°, 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 TURKSAT 2A’s average altitude, there are currently 28 active payloads and 14 tracked debris or rocket body fragments. Turkey operates approximately 41 active satellites in total.
❓ Frequently Asked Questions
TURKSAT 2A orbits at approximately 36,376 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 10,993 km/h — it just keeps pace with the ground below. With an inclination of 9.0°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
TURKSAT 2A is operated by Türksat (Turkey). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 26666. You can track TURKSAT 2A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
TURKSAT 2A was launched on 2001-01-10 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. View the full satellite launch log.
Yes — Orbital Radar tracks TURKSAT 2A (NORAD ID 26666) 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.
TURKSAT 2A travels at approximately 10,993 km/h (6,831 mph) — roughly 3.05 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.