YAOGAN-43 02C, 60947
Orbit data source: Space-Track
YAOGAN-43 02C, 60947 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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60947 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 YAOGAN-43 02C
1 60947U 24156C 25259.76367785 .00008886 00000-0 36968-3 0 9991
2 60947 34.9978 117.6977 0002509 51.5804 308.5136 15.23025725 57735Epoch: 2025-09-16T18:19Z
TLE epoch observation values (Epoch: 2025-09-16T18:19:41.766Z)
Latitude
0.00001°
Longitude
-153.17562°
Altitude
494.553 km
Speed
7.62 km/s
True Right ascension
07h 50m 47s
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
21:36:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.696 km
Perigee altitude
498.245 km
Semi-major axis
6,878.108 km
Eccentricity
0.00025
Inclination
34.9978°
RAAN
117.6977°
Arg. of periapsis
51.5804°
True anomaly
308.4911°
Mean anomaly
308.5136°
Eccentric anomaly
308.50235°
Mean motion
3.80487 °/min
Orbital period
94.62 mins
BSTAR
0.00036968
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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 02C 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 17:45:24.138Z | 204.323° SW | 2025-09-18 17:48:24.138Z | 151.39° SSE | 17.951° | 2025-09-18 17:50:24.138Z | 117.297° SE |
| 5 mins | 2025-09-18 19:25:24.138Z | 227.635° WSW | 2025-09-18 19:27:24.138Z | 173.144° S | 30.705° | 2025-09-18 19:30:24.138Z | 109.623° ESE |
| 5 mins | 2025-09-18 21:04:24.138Z | 246.291° WSW | 2025-09-18 21:06:24.138Z | 205.273° SW | 28.232° | 2025-09-18 21:09:24.138Z | 131.198° 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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