Skip to content
Home Library Satellite Directory HGS 1 (ASIASAT 3)

HGS 1 (ASIASAT 3)

NORAD 25126 Payload GEO 1997-086A ● Active
CONNECTING… GEO · NORAD 25126
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
35569 km
Apogee
36001 km
Inclination
13.2°
Period
1436.0 min
Mean Motion
1.00276997 rev/day
TLE Epoch
2026-06-19 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,785 km
Orbital Velocity11,070 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0051
Semi-Major Axis42,156 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 AsiaSat (United States)
Launch Date
1997-12-24
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1997-086A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
HGS 1 (ASIASAT 3) is an active satellite operated by AsiaSat (United States), launched on 1997-12-24 from Baikonur, Kazakhstan. With over 29 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,569 km and 36,001 km with an inclination of 13.2°. 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 HGS 1 (ASIASAT 3) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
HGS 1 (ASIASAT 3) 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 13.2°, 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 HGS 1 (ASIASAT 3)’s average altitude, there are currently 712 active payloads and 59 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. United States operates approximately 12,360 active satellites in total, of which 146 share a similar altitude band with HGS 1 (ASIASAT 3).
❓ Frequently Asked Questions
HGS 1 (ASIASAT 3) orbits at approximately 35,785 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. With an inclination of 13.2°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
HGS 1 (ASIASAT 3) is operated by AsiaSat (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25126. You can track HGS 1 (ASIASAT 3) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
HGS 1 (ASIASAT 3) was launched on 1997-12-24 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 HGS 1 (ASIASAT 3) (NORAD ID 25126) 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.
HGS 1 (ASIASAT 3) 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.