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APSTAR 6

NORAD 28638 Payload GEO 2005-012A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36231 km
Apogee
36309 km
Inclination
7.4°
Period
1460.9 min
Mean Motion
0.98572832 rev/day
TLE Epoch
2026-06-19 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,270 km
Orbital Velocity11,007 km/h
Velocity3.06 km/s
Orbital Period24.3 hours
Orbits / Day0.99
Eccentricity0.0009
Semi-Major Axis42,641 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 APT Satellite (China)
Launch Date
2005-04-12
Launch Site
Xichang, China
Int'l Designator
2005-012A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
APSTAR 6 is an active satellite operated by APT Satellite (China), launched on 2005-04-12 from Xichang, China. With over 21 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,231 km and 36,309 km with an inclination of 7.4°. It travels at approximately 11,007 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 APSTAR 6 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
APSTAR 6 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 7.4°, 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 APSTAR 6’s average altitude, there are currently 53 active payloads and 12 tracked debris or rocket body fragments. China operates approximately 1,218 active satellites in total, of which 2 share a similar altitude band with APSTAR 6.
❓ Frequently Asked Questions
APSTAR 6 orbits at approximately 36,270 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 11,007 km/h — it just keeps pace with the ground below. With an inclination of 7.4°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
APSTAR 6 is operated by APT Satellite (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 28638. You can track APSTAR 6 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
APSTAR 6 was launched on 2005-04-12 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks APSTAR 6 (NORAD ID 28638) 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.
APSTAR 6 travels at approximately 11,007 km/h (6,839 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.