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SHIYAN 3 (SY-3)

NORAD 33433 Payload LEO 2008-056A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
779 km
Apogee
800 km
Inclination
98.6°
Period
100.6 min
Mean Motion
14.30803031 rev/day
TLE Epoch
2026-06-19 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude790 km
Orbital Velocity26,860 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.31
Eccentricity0.0015
Semi-Major Axis7,161 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China Academy of Space Technology (CAST) (China)
Launch Date
2008-11-05
Launch Site
Jiuquan, China
Int'l Designator
2008-056A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
SHIYAN 3 (SY-3) is an active satellite operated by China Academy of Space Technology (CAST) (China), launched on 2008-11-05 from Jiuquan, China. After 18 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 779 km and 800 km with an inclination of 98.6°. It travels at approximately 26,860 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.31 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Orbital Radar tracks SHIYAN 3 (SY-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
SHIYAN 3 (SY-3) orbits at an average altitude of 790 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of SHIYAN 3 (SY-3)’s average altitude, there are currently 403 active payloads and 2,237 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 98.6°, SHIYAN 3 (SY-3) passes over latitudes between 98.6°N and 98.6°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. China operates approximately 1,219 active satellites in total, of which 77 share a similar altitude band with SHIYAN 3 (SY-3).
❓ Frequently Asked Questions
SHIYAN 3 (SY-3) is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 790 km altitude. Its 98.6° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 101 minutes, travelling at 26,860 km/h.
SHIYAN 3 (SY-3) is operated by China Academy of Space Technology (CAST) (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 33433. You can track SHIYAN 3 (SY-3) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SHIYAN 3 (SY-3) was launched on 2008-11-05 from Jiuquan, China, one of China’s oldest launch centres in the Gobi Desert, used for crewed Shenzhou missions and LEO satellites. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks SHIYAN 3 (SY-3) (NORAD ID 33433) 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.
SHIYAN 3 (SY-3) travels at approximately 26,860 km/h (16,690 mph) — roughly 7.46 km/s. It completes 14.31 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.