ASTRA 2B
NORAD 26494
Payload
GEO
2000-054A
● Active
CONNECTING…
GEO · NORAD 26494
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
36123 km
Apogee
36219 km
Inclination
9.6°
Period
1455.8 min
Mean Motion
0.98915821 rev/day
TLE Epoch
2026-06-19 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,171 km
Orbital Velocity11,020 km/h
Velocity3.06 km/s
Orbital Period24.3 hours
Orbits / Day0.99
Eccentricity0.0011
Semi-Major Axis42,542 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
SES S.A. (SES)
Launch Date
2000-09-14
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2000-054A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ASTRA 2B is an active satellite operated by SES S.A. (SES), launched on 2000-09-14 from Guiana Space Centre, Kourou. With over 26 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,123 km and 36,219 km with an inclination of 9.6°. It travels at approximately 11,020 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 2B 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 2B 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 9.6°, 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 2B’s average altitude, there are currently 155 active payloads and 11 tracked debris or rocket body fragments. SES operates approximately 77 active satellites in total, of which 16 share a similar altitude band with ASTRA 2B.
🔗 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 2B orbits at approximately 36,171 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 11,020 km/h — it just keeps pace with the ground below. With an inclination of 9.6°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
ASTRA 2B is operated by SES S.A. (SES). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 26494. You can track ASTRA 2B in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ASTRA 2B was launched on 2000-09-14 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 ASTRA 2B (NORAD ID 26494) 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 2B travels at approximately 11,020 km/h (6,847 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.