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YAOGAN-30 A

NORAD 42945 Payload LEO 2017-058A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
556 km
Apogee
559 km
Inclination
35.0°
Period
95.8 min
Mean Motion
15.03125465 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude558 km
Orbital Velocity27,306 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day15.03
Eccentricity0.0002
Semi-Major Axis6,929 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇨🇳 Chinese Ministry of National Defense (China)
Launch Date
2017-09-29
Launch Site
Xichang, China
Int'l Designator
2017-058A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
YAOGAN-30 A is an active satellite operated by Chinese Ministry of National Defense (China), launched on 2017-09-29 from Xichang, China. It orbits in Low Earth Orbit (LEO) at altitudes between 556 km and 559 km with an inclination of 35.0°. It travels at approximately 27,306 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 15.03 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-30 A 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 A orbits at an average altitude of 558 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-30 A’s average altitude, there are currently 3,296 active payloads and 406 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, ONEWEB-0050. This makes it one of the more crowded altitude bands, containing roughly 18.9% of all active satellites. With an inclination of 35.0°, YAOGAN-30 A 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 154 share a similar altitude band with YAOGAN-30 A.
🔗 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 A orbits in Low Earth Orbit (LEO) at altitudes between 556 km (perigee) and 559 km (apogee), with an average altitude of approximately 558 km. It completes one orbit every 96 minutes, travelling at approximately 27,306 km/h (16,967 mph).
YAOGAN-30 A is operated by Chinese Ministry of National Defense (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 42945. You can track YAOGAN-30 A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
YAOGAN-30 A was launched on 2017-09-29 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-30 A (NORAD ID 42945) 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 A travels at approximately 27,306 km/h (16,967 mph) — roughly 7.58 km/s. It completes 15.03 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.