SHIYAN 23 (SY-23)
NORAD 59728
Payload
LEO
2024-089A
● Active
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LEO · NORAD 59728
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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
605 km
Apogee
610 km
Inclination
97.8°
Period
96.8 min
Mean Motion
14.87035008 rev/day
TLE Epoch
2026-06-17 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude608 km
Orbital Velocity27,208 km/h
Velocity7.56 km/s
Orbital Period97 minutes
Orbits / Day14.87
Eccentricity0.0004
Semi-Major Axis6,979 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2024-05-11
Launch Site
Jiuquan, China
Int'l Designator
2024-089A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
SHIYAN 23 (SY-23) is an active satellite operated by China, launched on 2024-05-11 from Jiuquan, China. It orbits in Low Earth Orbit (LEO) at altitudes between 605 km and 610 km with an inclination of 97.8°. It travels at approximately 27,208 km/h (7.56 km/s), completing one full orbit every 97 minutes — that’s roughly 14.87 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. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. Orbital Radar tracks SHIYAN 23 (SY-23) 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 23 (SY-23) orbits at an average altitude of 608 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 23 (SY-23)’s average altitude, there are currently 1,624 active payloads and 698 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3090. This makes it one of the more crowded altitude bands, containing roughly 9.3% of all active satellites. With an inclination of 97.8°, SHIYAN 23 (SY-23) passes over latitudes between 97.8°N and 97.8°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 172 share a similar altitude band with SHIYAN 23 (SY-23).
❓ Frequently Asked Questions
SHIYAN 23 (SY-23) is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 608 km altitude. Its 97.8° 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 97 minutes, travelling at 27,208 km/h.
SHIYAN 23 (SY-23) is operated by China. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 59728. You can track SHIYAN 23 (SY-23) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SHIYAN 23 (SY-23) was launched on 2024-05-11 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks SHIYAN 23 (SY-23) (NORAD ID 59728) 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 23 (SY-23) travels at approximately 27,208 km/h (16,906 mph) — roughly 7.56 km/s. It completes 14.87 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.