YAOGAN 4
NORAD 33446
Payload
LEO
2008-061A
● Active
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LEO · NORAD 33446
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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
608 km
Apogee
630 km
Inclination
97.9°
Period
97.1 min
Mean Motion
14.83203506 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude619 km
Orbital Velocity27,185 km/h
Velocity7.55 km/s
Orbital Period97 minutes
Orbits / Day14.83
Eccentricity0.0016
Semi-Major Axis6,990 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇨🇳 Chinese Ministry of National Defense (China)
Launch Date
2008-12-01
Launch Site
Jiuquan, China
Int'l Designator
2008-061A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
YAOGAN 4 is an active satellite operated by Chinese Ministry of National Defense (China), launched on 2008-12-01 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 608 km and 630 km with an inclination of 97.9°. It travels at approximately 27,185 km/h (7.55 km/s), completing one full orbit every 97 minutes — that’s roughly 14.83 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 ~10–25 years. Orbital Radar tracks YAOGAN 4 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 4 orbits at an average altitude of 619 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 4’s average altitude, there are currently 1,548 active payloads and 761 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3090, STARLINK-3077. This makes it one of the more crowded altitude bands, containing roughly 8.9% of all active satellites. With an inclination of 97.9°, YAOGAN 4 passes over latitudes between 97.9°N and 97.9°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 134 share a similar altitude band with YAOGAN 4.
🔗 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 4 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 619 km altitude. Its 97.9° 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 27,185 km/h.
YAOGAN 4 is operated by Chinese Ministry of National Defense (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 33446. You can track YAOGAN 4 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
YAOGAN 4 was launched on 2008-12-01 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 YAOGAN 4 (NORAD ID 33446) 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 4 travels at approximately 27,185 km/h (16,892 mph) — roughly 7.55 km/s. It completes 14.83 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.