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YAOGAN-43 O1A

NORAD 60458 Payload LEO 2024-148A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
455 km
Apogee
463 km
Inclination
35.0°
Period
93.8 min
Mean Motion
15.35732357 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude459 km
Orbital Velocity27,502 km/h
Velocity7.64 km/s
Orbital Period94 minutes
Orbits / Day15.36
Eccentricity0.0006
Semi-Major Axis6,830 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇨🇳 PLA Strategic Support Force (China)
Launch Date
2024-08-16
Launch Site
Xichang, China
Int'l Designator
2024-148A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
YAOGAN-43 O1A is an active satellite operated by PLA Strategic Support Force (China), launched on 2024-08-16 from Xichang, China. It orbits in Low Earth Orbit (LEO) at altitudes between 455 km and 463 km with an inclination of 35.0°. It travels at approximately 27,502 km/h (7.64 km/s), completing one full orbit every 94 minutes — that’s roughly 15.36 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 ~1–3 years. Orbital Radar tracks YAOGAN-43 O1A 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-43 O1A orbits at an average altitude of 459 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-43 O1A’s average altitude, there are currently 7,901 active payloads and 168 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1017. This makes it one of the more crowded altitude bands, containing roughly 45.4% of all active satellites. With an inclination of 35.0°, YAOGAN-43 O1A 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 150 share a similar altitude band with YAOGAN-43 O1A.
🔗 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-43 O1A orbits in Low Earth Orbit (LEO) at altitudes between 455 km (perigee) and 463 km (apogee), with an average altitude of approximately 459 km. It completes one orbit every 94 minutes, travelling at approximately 27,502 km/h (17,089 mph).
YAOGAN-43 O1A is operated by PLA Strategic Support Force (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 60458. You can track YAOGAN-43 O1A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
YAOGAN-43 O1A was launched on 2024-08-16 from Xichang, China. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks YAOGAN-43 O1A (NORAD ID 60458) 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-43 O1A travels at approximately 27,502 km/h (17,089 mph) — roughly 7.64 km/s. It completes 15.36 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.