YAOGAN-43 O1J, 60466
Orbit data source: Space-Track
YAOGAN-43 O1J, 60466 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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60466 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: 14 hours ago
TLE from 14 hours ago
0 YAOGAN-43 O1J
1 60466U 24148J 26136.90980956 .00011560 00000-0 32614-3 0 9997
2 60466 34.9930 334.3450 0008733 332.4727 27.5529 15.35535214 97621Epoch: 2026-05-16T21:50Z
TLE epoch observation values (Epoch: 2026-05-16T21:50:07.545Z)
Latitude
0.00001°
Longitude
132.19357°
Altitude
452.94 km
Speed
7.646 km/s
True Right ascension
22h 17m 22s
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
20:21:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.574 km
Perigee altitude
456.626 km
Semi-major axis
6,840.737 km
Eccentricity
0.00087
Inclination
34.993°
RAAN
334.345°
Arg. of periapsis
332.4727°
True anomaly
27.59924°
Mean anomaly
27.5529°
Eccentric anomaly
27.57606°
Mean motion
3.83609 °/min
Orbital period
93.85 mins
BSTAR
0.00032614
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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 O1J 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 16:47:32.711Z | 199.024° SSW | 2026-05-17 16:49:32.711Z | 164.632° S | 16.071° | 2026-05-17 16:51:32.711Z | 126.074° SE |
| 5 mins | 2026-05-17 18:26:32.711Z | 223.331° SW | 2026-05-17 18:28:32.711Z | 164.061° S | 28.886° | 2026-05-17 18:31:32.711Z | 107.632° ESE |
| 4 mins | 2026-05-17 20:05:32.711Z | 230.643° WSW | 2026-05-17 20:06:32.711Z | 202.817° SW | 27.746° | 2026-05-17 20:09:32.711Z | 128.819° 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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