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YAOGAN-50 02

NORAD 68196 Payload LEO 2026-051A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
952 km
Apogee
953 km
Inclination
142.0°
Period
104.1 min
Mean Motion
13.83269892 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude953 km
Orbital Velocity26,559 km/h
Velocity7.38 km/s
Orbital Period104 minutes
Orbits / Day13.83
Eccentricity0.0001
Semi-Major Axis7,324 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 PLA Strategic Support Force (China)
Launch Date
2026-03-15
Launch Site
Taiyuan, China
Int'l Designator
2026-051A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
YAOGAN-50 02 is an active satellite operated by PLA Strategic Support Force (China), launched on 2026-03-15 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 952 km and 953 km with an inclination of 142.0°. It travels at approximately 26,559 km/h (7.38 km/s), completing one full orbit every 104 minutes — that’s roughly 13.83 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-50 02 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 02 orbits at an average altitude of 953 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 02’s average altitude, there are currently 303 active payloads and 1,080 tracked debris or rocket body fragments. With an inclination of 142.0°, YAOGAN-50 02 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 1,219 active satellites in total, of which 28 share a similar altitude band with YAOGAN-50 02.
🔗 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 02 orbits in Low Earth Orbit (LEO) at altitudes between 952 km (perigee) and 953 km (apogee), with an average altitude of approximately 953 km. It completes one orbit every 104 minutes, travelling at approximately 26,559 km/h (16,503 mph).
YAOGAN-50 02 is operated by PLA Strategic Support Force (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 68196. You can track YAOGAN-50 02 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
YAOGAN-50 02 was launched on 2026-03-15 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-50 02 (NORAD ID 68196) 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-50 02 travels at approximately 26,559 km/h (16,503 mph) — roughly 7.38 km/s. It completes 13.83 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.