YAOGAN-43 O1D
NORAD 60461
Payload
LEO
2024-148D
● Active
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LEO · NORAD 60461
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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
474 km
Apogee
478 km
Inclination
35.0°
Period
94.1 min
Mean Motion
15.29872651 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude476 km
Orbital Velocity27,468 km/h
Velocity7.63 km/s
Orbital Period94 minutes
Orbits / Day15.30
Eccentricity0.0003
Semi-Major Axis6,847 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
2024-148D
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
YAOGAN-43 O1D 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 474 km and 478 km with an inclination of 35.0°. It travels at approximately 27,468 km/h (7.63 km/s), completing one full orbit every 94 minutes — that’s roughly 15.30 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 O1D 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 O1D orbits at an average altitude of 476 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 O1D’s average altitude, there are currently 7,964 active payloads and 204 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 45.7% of all active satellites. With an inclination of 35.0°, YAOGAN-43 O1D 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 178 share a similar altitude band with YAOGAN-43 O1D.
🔗 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 O1D orbits in Low Earth Orbit (LEO) at altitudes between 474 km (perigee) and 478 km (apogee), with an average altitude of approximately 476 km. It completes one orbit every 94 minutes, travelling at approximately 27,468 km/h (17,068 mph).
YAOGAN-43 O1D is operated by PLA Strategic Support Force (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 60461. You can track YAOGAN-43 O1D in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
YAOGAN-43 O1D 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 O1D (NORAD ID 60461) 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 O1D travels at approximately 27,468 km/h (17,068 mph) — roughly 7.63 km/s. It completes 15.30 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.