CHINASAT 9A
NORAD 42763
Payload
GEO
2017-035A
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GEO · NORAD 42763
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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
35906 km
Apogee
35943 km
Inclination
5.0°
Period
1443.2 min
Mean Motion
0.99781875 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,925 km
Orbital Velocity11,052 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0004
Semi-Major Axis42,296 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China Satellite Communications (China)
Launch Date
2017-06-18
Launch Site
Xichang, China
Int'l Designator
2017-035A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
CHINASAT 9A is an active satellite operated by China Satellite Communications (China), launched on 2017-06-18 from Xichang, China. It orbits in Geostationary Orbit (GEO) at altitudes between 35,906 km and 35,943 km with an inclination of 5.0°. It travels at approximately 11,052 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 9A 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 9A 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 5.0°, 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 9A’s average altitude, there are currently 60 active payloads and 16 tracked debris or rocket body fragments. China operates approximately 1,219 active satellites in total, of which 4 share a similar altitude band with CHINASAT 9A.
❓ Frequently Asked Questions
CHINASAT 9A orbits at approximately 35,925 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 11,052 km/h — it just keeps pace with the ground below. With an inclination of 5.0°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
CHINASAT 9A is operated by China Satellite Communications (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 42763. You can track CHINASAT 9A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CHINASAT 9A was launched on 2017-06-18 from Xichang, China. View the full satellite launch log.
Yes — Orbital Radar tracks CHINASAT 9A (NORAD ID 42763) 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 9A travels at approximately 11,052 km/h (6,867 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.