YAOGAN-47
NORAD 66988
Payload
LEO
2025-289A
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LEO · NORAD 66988
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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
494 km
Apogee
497 km
Inclination
97.5°
Period
94.5 min
Mean Motion
15.23403411 rev/day
TLE Epoch
2026-09-17 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude496 km
Orbital Velocity27,429 km/h
Velocity7.62 km/s
Orbital Period95 minutes
Orbits / Day15.23
Eccentricity0.0002
Semi-Major Axis6,867 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇨🇳 CASC? (China)
Launch Date
2025-12-09
Launch Site
Jiuquan Satellite Launch Center, China
Int'l Designator
2025-289A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
YAOGAN-47 is an active satellite operated by CASC? (China), launched on 2025-12-09 from Jiuquan Satellite Launch Center, China on the Yaogan 47 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 494 km and 497 km with an inclination of 97.5°. It travels at approximately 27,429 km/h (7.62 km/s), completing one full orbit every 95 minutes — that’s roughly 15.23 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 ~1–3 years. Orbital Radar tracks YAOGAN-47 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
YAOGAN-47 orbits at an average altitude of 496 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 YAOGAN-47’s average altitude, there are currently 10,269 active payloads and 221 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 54.9% of all active satellites. With an inclination of 97.5°, YAOGAN-47 passes over latitudes between 97.5°N and 97.5°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 1,275 active satellites in total, of which 193 share a similar altitude band with YAOGAN-47.
🔗 Yaogan Reconnaissance Series
This satellite is part of China's Yaogan series, officially described as “remote sensing” satellites but widely assessed by analysts to serve military reconnaissance, signals intelligence and ocean surveillance missions. The series includes optical imaging, synthetic aperture radar (SAR) and electronic intelligence (ELINT) variants, some operating in coordinated orbital formations for persistent maritime monitoring.
❓ Frequently Asked Questions
YAOGAN-47 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 496 km altitude. Its 97.5° 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 95 minutes, travelling at 27,429 km/h.
YAOGAN-47 is operated by CASC? (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 66988. You can track YAOGAN-47 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
YAOGAN-47 was launched on 2025-12-09 from Jiuquan Satellite Launch Center, 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: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks YAOGAN-47 (NORAD ID 66988) 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.
YAOGAN-47 travels at approximately 27,429 km/h (17,043 mph) — roughly 7.62 km/s. It completes 15.23 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.