ASTRA 1H
NORAD 25785
Payload
GEO
1999-033A
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GEO · NORAD 25785
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
36126 km
Apogee
36199 km
Inclination
10.6°
Period
1455.3 min
Mean Motion
0.98945952 rev/day
TLE Epoch
2026-06-19 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,163 km
Orbital Velocity11,021 km/h
Velocity3.06 km/s
Orbital Period24.3 hours
Orbits / Day0.99
Eccentricity0.0009
Semi-Major Axis42,534 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
SES S.A. (SES)
Launch Date
1999-06-18
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1999-033A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ASTRA 1H is an active satellite operated by SES S.A. (SES), launched on 1999-06-18 from Baikonur, Kazakhstan. With over 27 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,126 km and 36,199 km with an inclination of 10.6°. 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 ASTRA 1H 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 1H 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 10.6°, 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 1H’s average altitude, there are currently 156 active payloads and 9 tracked debris or rocket body fragments. SES operates approximately 77 active satellites in total, of which 20 share a similar altitude band with ASTRA 1H.
🔗 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 1H orbits at approximately 36,163 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 10.6°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
ASTRA 1H is operated by SES S.A. (SES). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25785. You can track ASTRA 1H in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ASTRA 1H was launched on 1999-06-18 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 1H (NORAD ID 25785) 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 1H 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.