Skip to content
Home Library Satellite Directory YAOGAN 30

YAOGAN 30

NORAD 41473 Payload LEO 2016-029A ● Active
CONNECTING… LEO · NORAD 41473
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
631 km
Apogee
651 km
Inclination
97.9°
Period
97.5 min
Mean Motion
14.76271565 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude641 km
Orbital Velocity27,143 km/h
Velocity7.54 km/s
Orbital Period98 minutes
Orbits / Day14.76
Eccentricity0.0014
Semi-Major Axis7,012 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇨🇳 Chinese Ministry of National Defense (China)
Launch Date
2016-05-15
Launch Site
Jiuquan, China
Int'l Designator
2016-029A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
YAOGAN 30 is an active satellite operated by Chinese Ministry of National Defense (China), launched on 2016-05-15 from Jiuquan, China. After 10 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 631 km and 651 km with an inclination of 97.9°. It travels at approximately 27,143 km/h (7.54 km/s), completing one full orbit every 98 minutes — that’s roughly 14.76 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 30 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 30 orbits at an average altitude of 641 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 30’s average altitude, there are currently 737 active payloads and 933 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, ONEWEB-0050. With an inclination of 97.9°, YAOGAN 30 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 159 share a similar altitude band with YAOGAN 30.
🔗 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 30 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 641 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 98 minutes, travelling at 27,143 km/h.
YAOGAN 30 is operated by Chinese Ministry of National Defense (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 41473. You can track YAOGAN 30 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
YAOGAN 30 was launched on 2016-05-15 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 30 (NORAD ID 41473) 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 30 travels at approximately 27,143 km/h (16,866 mph) — roughly 7.54 km/s. It completes 14.76 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.