YAOGAN-40 02C
NORAD 63920
Payload
LEO
2025-096C
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LEO · NORAD 63920
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🛰️ Orbital Parameters
Perigee
849 km
Apogee
853 km
Inclination
86.0°
Period
102.0 min
Mean Motion
14.12448515 rev/day
TLE Epoch
2026-06-19 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude851 km
Orbital Velocity26,745 km/h
Velocity7.43 km/s
Orbital Period102 minutes
Orbits / Day14.12
Eccentricity0.0003
Semi-Major Axis7,222 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 PLA Strategic Support Force (China)
Launch Date
2025-05-11
Launch Site
Taiyuan, China
Int'l Designator
2025-096C
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
YAOGAN-40 02C is an active satellite operated by PLA Strategic Support Force (China), launched on 2025-05-11 from Taiyuan, China. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 849 km and 853 km with an inclination of 86.0°. It travels at approximately 26,745 km/h (7.43 km/s), completing one full orbit every 102 minutes — that’s roughly 14.12 orbits per day. 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 ~100–500 years. Orbital Radar tracks YAOGAN-40 02C 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-40 02C orbits at an average altitude of 851 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-40 02C’s average altitude, there are currently 268 active payloads and 2,031 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 86.0°, YAOGAN-40 02C passes over latitudes between 86.0°N and 86.0°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 1,219 active satellites in total, of which 138 share a similar altitude band with YAOGAN-40 02C.
🔗 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-40 02C orbits in Low Earth Orbit (LEO) at altitudes between 849 km (perigee) and 853 km (apogee), with an average altitude of approximately 851 km. It completes one orbit every 102 minutes, travelling at approximately 26,745 km/h (16,619 mph).
YAOGAN-40 02C is operated by PLA Strategic Support Force (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 63920. You can track YAOGAN-40 02C in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
YAOGAN-40 02C was launched on 2025-05-11 from Taiyuan, 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-40 02C (NORAD ID 63920) 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-40 02C travels at approximately 26,745 km/h (16,619 mph) — roughly 7.43 km/s. It completes 14.12 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.