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ANGOSAT 1

NORAD 43087 Payload GEO 2017-086A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35962 km
Apogee
36114 km
Inclination
7.6°
Period
1449.0 min
Mean Motion
0.99381866 rev/day
TLE Epoch
2026-06-18 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,038 km
Orbital Velocity11,037 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day0.99
Eccentricity0.0018
Semi-Major Axis42,409 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
AGO
Launch Date
2017-12-26
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2017-086A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ANGOSAT 1 is an active satellite operated by AGO, launched on 2017-12-26 from Baikonur, Kazakhstan. It orbits in Geostationary Orbit (GEO) at altitudes between 35,962 km and 36,114 km with an inclination of 7.6°. It travels at approximately 11,037 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — 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 ANGOSAT 1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ANGOSAT 1 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 7.6°, 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 ANGOSAT 1’s average altitude, there are currently 81 active payloads and 27 tracked debris or rocket body fragments. AGO operates approximately 2 active satellites in total.
❓ Frequently Asked Questions
ANGOSAT 1 orbits at approximately 36,038 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 11,037 km/h — it just keeps pace with the ground below. With an inclination of 7.6°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
ANGOSAT 1 is operated by AGO. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 43087. You can track ANGOSAT 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ANGOSAT 1 was launched on 2017-12-26 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 ANGOSAT 1 (NORAD ID 43087) 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.
ANGOSAT 1 travels at approximately 11,037 km/h (6,858 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.