Skip to content
Home Library Satellite Directory ASTRA 2G

ASTRA 2G

NORAD 40364 Payload GEO 2014-089A ● Active
CONNECTING… GEO · NORAD 40364
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
35768 km
Apogee
35807 km
Inclination
0.1°
Period
1436.2 min
Mean Motion
1.00268810 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,788 km
Orbital Velocity11,070 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0005
Semi-Major Axis42,159 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
SES S.A. (SES)
Launch Date
2014-12-27
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2014-089A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ASTRA 2G is an active satellite operated by SES S.A. (SES), launched on 2014-12-27 from Baikonur, Kazakhstan. After 12 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 35,768 km and 35,807 km with an inclination of 0.1°. It travels at approximately 11,070 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 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 2G 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 2G 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. Within ±50 km of ASTRA 2G’s average altitude, there are currently 714 active payloads and 60 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. SES operates approximately 77 active satellites in total, of which 36 share a similar altitude band with ASTRA 2G.
🔗 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 2G orbits at approximately 35,788 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 11,070 km/h — it just keeps pace with the ground below. Learn more about geostationary orbits.
ASTRA 2G is operated by SES S.A. (SES). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 40364. You can track ASTRA 2G in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ASTRA 2G was launched on 2014-12-27 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 2G (NORAD ID 40364) 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 2G travels at approximately 11,070 km/h (6,878 mph) — roughly 3.07 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.