YAOGAN-43 02B, 60946
Orbit data source: Space-Track
YAOGAN-43 02B, 60946 is a payload satellite owned by PLA GAD (CN) in LEO that was launched on Tue, 03 Sep 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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60946 intel report (Beta)
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Edit Public Description
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: 3 days ago
TLE from 3 days ago
0 YAOGAN-43 02B
1 60946U 24156B 25258.06080208 .00011836 00000-0 49120-3 0 9997
2 60946 34.9923 128.2757 0001914 289.7862 70.2646 15.23058522 57477Epoch: 2025-09-15T01:27Z
TLE epoch observation values (Epoch: 2025-09-15T01:27:33.299Z)
Latitude
-0.00003°
Longitude
112.11604°
Altitude
495.084 km
Speed
7.62 km/s
True Right ascension
08h 33m 06s
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
16:07:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.189 km
Perigee altitude
498.557 km
Semi-major axis
6,878.01 km
Eccentricity
0.00019
Inclination
34.9923°
RAAN
128.2757°
Arg. of periapsis
289.7862°
True anomaly
70.28525°
Mean anomaly
70.2646°
Eccentric anomaly
70.27492°
Mean motion
3.80495 °/min
Orbital period
94.61 mins
BSTAR
0.0004912
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Other satellites on launch #156 in the year 2024 (2024-09-03 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 02B 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-18 17:47:13.859Z | 206.626° SW | 2025-09-18 17:50:13.859Z | 154.676° SSE | 18.512° | 2025-09-18 17:52:13.859Z | 118.943° SE |
| 5 mins | 2025-09-18 19:27:13.859Z | 230.115° WSW | 2025-09-18 19:29:13.859Z | 179.271° S | 30.852° | 2025-09-18 19:32:13.859Z | 110.948° ESE |
| 5 mins | 2025-09-18 21:07:13.859Z | 234.344° WSW | 2025-09-18 21:09:13.859Z | 175.585° S | 28.226° | 2025-09-18 21:12:13.859Z | 124.955° 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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