YAOGAN-39 01B
NORAD 57728
Payload
LEO
2023-130B
● Active
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LEO · NORAD 57728
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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
512 km
Apogee
523 km
Inclination
35.0°
Period
95.0 min
Mean Motion
15.16273314 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude518 km
Orbital Velocity27,385 km/h
Velocity7.61 km/s
Orbital Period95 minutes
Orbits / Day15.16
Eccentricity0.0008
Semi-Major Axis6,889 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇨🇳 PLA Strategic Support Force (China)
Launch Date
2023-08-31
Launch Site
Xichang, China
Int'l Designator
2023-130B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
YAOGAN-39 01B is an active satellite operated by PLA Strategic Support Force (China), launched on 2023-08-31 from Xichang, China. It orbits in Low Earth Orbit (LEO) at altitudes between 512 km and 523 km with an inclination of 35.0°. It travels at approximately 27,385 km/h (7.61 km/s), completing one full orbit every 95 minutes — that’s roughly 15.16 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 ~3–10 years. Orbital Radar tracks YAOGAN-39 01B 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-39 01B orbits at an average altitude of 518 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of YAOGAN-39 01B’s average altitude, there are currently 7,737 active payloads and 276 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1184. This makes it one of the more crowded altitude bands, containing roughly 44.4% of all active satellites. With an inclination of 35.0°, YAOGAN-39 01B passes over latitudes between 35.0°N and 35.0°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. China operates approximately 1,219 active satellites in total, of which 219 share a similar altitude band with YAOGAN-39 01B.
🔗 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-39 01B orbits in Low Earth Orbit (LEO) at altitudes between 512 km (perigee) and 523 km (apogee), with an average altitude of approximately 518 km. It completes one orbit every 95 minutes, travelling at approximately 27,385 km/h (17,016 mph).
YAOGAN-39 01B is operated by PLA Strategic Support Force (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 57728. You can track YAOGAN-39 01B in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
YAOGAN-39 01B was launched on 2023-08-31 from Xichang, China. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks YAOGAN-39 01B (NORAD ID 57728) 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-39 01B travels at approximately 27,385 km/h (17,016 mph) — roughly 7.61 km/s. It completes 15.16 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.