CHINASAT 22A
NORAD 29398
Payload
GEO
2006-038A
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GEO · NORAD 29398
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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
35824 km
Apogee
35842 km
Inclination
11.5°
Period
1438.5 min
Mean Motion
1.00106339 rev/day
TLE Epoch
2026-06-19 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,833 km
Orbital Velocity11,064 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0002
Semi-Major Axis42,204 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China Satellite Communications (China)
Launch Date
2006-09-12
Launch Site
Xichang, China
Int'l Designator
2006-038A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
CHINASAT 22A is an active satellite operated by China Satellite Communications (China), launched on 2006-09-12 from Xichang, China. With over 20 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,824 km and 35,842 km with an inclination of 11.5°. It travels at approximately 11,064 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 CHINASAT 22A in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
CHINASAT 22A 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 11.5°, 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 CHINASAT 22A’s average altitude, there are currently 680 active payloads and 55 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. China operates approximately 1,218 active satellites in total, of which 109 share a similar altitude band with CHINASAT 22A.
❓ Frequently Asked Questions
CHINASAT 22A orbits at approximately 35,833 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 11,064 km/h — it just keeps pace with the ground below. With an inclination of 11.5°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
CHINASAT 22A is operated by China Satellite Communications (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 29398. You can track CHINASAT 22A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CHINASAT 22A was launched on 2006-09-12 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks CHINASAT 22A (NORAD ID 29398) 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.
CHINASAT 22A travels at approximately 11,064 km/h (6,875 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.