YAOGAN-50 30
NORAD 101149
Payload
LEO
2026-240A
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LEO · NORAD 101149
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Longitude
🛰️ Orbital Parameters
Perigee
701 km
Apogee
945 km
Inclination
142.0°
Period
101.4 min
Mean Motion
14.20636455 rev/day
TLE Epoch
2026-10-23 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude823 km
Orbital Velocity26,797 km/h
Velocity7.44 km/s
Orbital Period101 minutes
Orbits / Day14.21
Eccentricity0.0170
Semi-Major Axis7,194 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 PLA Strategic Support Force (China)
Launch Date
2026-10-23
Launch Site
Taiyuan Satellite Launch Center, China
Int'l Designator
2026-240A
Object Type
Payload
RCS Size
Unknown
📖 About This Object
YAOGAN-50 30 is an active satellite operated by PLA Strategic Support Force (China), launched on 2026-10-23 from Taiyuan Satellite Launch Center, China on the Yaogan 50-03 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 701 km and 945 km with an inclination of 142.0°. It travels at approximately 26,797 km/h (7.44 km/s), completing one full orbit every 101 minutes — that’s roughly 14.21 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks YAOGAN-50 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-50 30 orbits at an average altitude of 823 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of YAOGAN-50 30’s average altitude, there are currently 402 active payloads and 2,501 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0455. With an inclination of 142.0°, YAOGAN-50 30 passes over latitudes between 142.0°N and 142.0°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 1,340 active satellites in total, of which 86 share a similar altitude band with YAOGAN-50 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-50 30 orbits in Low Earth Orbit (LEO) at altitudes between 701 km (perigee) and 945 km (apogee), with an average altitude of approximately 823 km. It completes one orbit every 101 minutes, travelling at approximately 26,797 km/h (16,651 mph).
YAOGAN-50 30 is operated by PLA Strategic Support Force (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 101149. You can track YAOGAN-50 30 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
YAOGAN-50 30 was launched on 2026-10-23 from Taiyuan Satellite Launch Center, China. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks YAOGAN-50 30 (NORAD ID 101149) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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-50 30 travels at approximately 26,797 km/h (16,651 mph) — roughly 7.44 km/s. It completes 14.21 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.