ASTRA 2D
NORAD 26638
Payload
GEO
2000-081A
● Active
CONNECTING…
GEO · NORAD 26638
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
36141 km
Apogee
36154 km
Inclination
10.5°
Period
1454.6 min
Mean Motion
0.98999507 rev/day
TLE Epoch
2026-06-19 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,148 km
Orbital Velocity11,023 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0002
Semi-Major Axis42,519 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
SES S.A. (SES)
Launch Date
2000-12-20
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2000-081A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ASTRA 2D is an active satellite operated by SES S.A. (SES), launched on 2000-12-20 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 36,141 km and 36,154 km with an inclination of 10.5°. It travels at approximately 11,023 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 2D 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 2D 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 10.5°, 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 2D’s average altitude, there are currently 173 active payloads and 9 tracked debris or rocket body fragments. SES operates approximately 77 active satellites in total, of which 23 share a similar altitude band with ASTRA 2D.
🔗 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 2D orbits at approximately 36,148 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 11,023 km/h — it just keeps pace with the ground below. With an inclination of 10.5°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
ASTRA 2D is operated by SES S.A. (SES). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 26638. You can track ASTRA 2D in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ASTRA 2D was launched on 2000-12-20 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 2D (NORAD ID 26638) 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 2D travels at approximately 11,023 km/h (6,849 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.