YAOGAN-43 O1G, 60464
Orbit data source: Space-Track
YAOGAN-43 O1G, 60464 is a payload satellite owned by PLA GAD (CN) in LEO that was launched on Fri, 16 Aug 2024 UTC via a CHANG ZHENG 4B launch vehicle from the Xichang Space Center, China (XSC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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60464 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Operational Defense Communications
Bus & Motor
Unknown
Mass
~300 kg wet, ~300 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.5 m
Radar Cross Section
11.063 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 YAOGAN-43 O1G
1 60464U 24148G 26136.94065944 .00005129 00000-0 17654-3 0 9991
2 60464 35.0061 347.3259 0006796 227.9926 132.0213 15.29394734 97493Epoch: 2026-05-16T22:34Z
TLE epoch observation values (Epoch: 2026-05-16T22:34:32.975Z)
Latitude
0.00001°
Longitude
134.0381°
Altitude
479.645 km
Speed
7.626 km/s
True Right ascension
23h 09m 18s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
20:22:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.54 km
Perigee altitude
476.217 km
Semi-major axis
6,859.016 km
Eccentricity
0.00068
Inclination
35.0061°
RAAN
347.3259°
Arg. of periapsis
227.9926°
True anomaly
132.07912°
Mean anomaly
132.0213°
Eccentric anomaly
132.05021°
Mean motion
3.82077 °/min
Orbital period
94.22 mins
BSTAR
0.00017654
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Other satellites on launch #148 in the year 2024 (2024-08-16 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.YAOGAN-43 O1G Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-17 17:37:02.753Z | 189.708° SSW | 2026-05-17 17:39:02.753Z | 151.757° SSE | 16.492° | 2026-05-17 17:41:02.753Z | 118.19° SE |
| 5 mins | 2026-05-17 19:16:02.753Z | 219.488° SW | 2026-05-17 19:18:02.753Z | 157.159° SSE | 29.01° | 2026-05-17 19:21:02.753Z | 106.372° ESE |
| 5 mins | 2026-05-17 20:55:02.753Z | 235.079° WSW | 2026-05-17 20:57:02.753Z | 174.536° S | 28.766° | 2026-05-17 21:00:02.753Z | 122.361° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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