EUTE 16C (SESAT 1)
NORAD 26243
Payload
GEO
2000-019A
● Active
CONNECTING…
GEO · NORAD 26243
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
36144 km
Apogee
36177 km
Inclination
10.9°
Period
1455.2 min
Mean Motion
0.98952851 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,161 km
Orbital Velocity11,021 km/h
Velocity3.06 km/s
Orbital Period24.3 hours
Orbits / Day0.99
Eccentricity0.0004
Semi-Major Axis42,532 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
Eutelsat
Launch Date
2000-04-17
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2000-019A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
EUTE 16C (SESAT 1) is an active satellite operated by Eutelsat, launched on 2000-04-17 from Baikonur, Kazakhstan. With over 26 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,144 km and 36,177 km with an inclination of 10.9°. It travels at approximately 11,021 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 EUTE 16C (SESAT 1) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
EUTE 16C (SESAT 1) 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 10.9°, 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 EUTE 16C (SESAT 1)’s average altitude, there are currently 162 active payloads and 9 tracked debris or rocket body fragments. Eutelsat operates approximately 62 active satellites in total, of which 10 share a similar altitude band with EUTE 16C (SESAT 1).
❓ Frequently Asked Questions
EUTE 16C (SESAT 1) orbits at approximately 36,161 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 11,021 km/h — it just keeps pace with the ground below. With an inclination of 10.9°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
EUTE 16C (SESAT 1) is operated by Eutelsat. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 26243. You can track EUTE 16C (SESAT 1) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
EUTE 16C (SESAT 1) was launched on 2000-04-17 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 EUTE 16C (SESAT 1) (NORAD ID 26243) 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.
EUTE 16C (SESAT 1) travels at approximately 11,021 km/h (6,848 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.