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: 20 hours ago
TLE from 20 hours ago
0 YAOGAN-43 02C
1 60947U 24156C 25300.99511297 .00012717 00000-0 52752-3 0 9999
2 60947 34.9972 218.3893 0001840 34.4295 325.6539 15.23064490 64025Epoch: 2025-10-27T23:52Z
TLE epoch observation values (Epoch: 2025-10-27T23:52:57.760Z)
Latitude
-0°
Longitude
-176.44033°
Altitude
494.466 km
Speed
7.62 km/s
True Right ascension
14h 33m 33s
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
15:15:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.12 km
Perigee altitude
498.589 km
Semi-major axis
6,877.991 km
Eccentricity
0.00018
Inclination
34.9972°
RAAN
218.3893°
Arg. of periapsis
34.4295°
True anomaly
325.642°
Mean anomaly
325.6539°
Eccentric anomaly
325.64795°
Mean motion
3.80497 °/min
Orbital period
94.61 mins
BSTAR
0.00052752
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-28 22:08:33.915Z | 194.601° SSW | 2025-10-28 22:10:33.915Z | 159.251° S | 16.939° | 2025-10-28 22:12:33.915Z | 123.145° SE |
| 5 mins | 2025-10-28 23:47:33.915Z | 230.347° WSW | 2025-10-28 23:49:33.915Z | 186.703° SSW | 29.545° | 2025-10-28 23:52:33.915Z | 112.437° ESE |
| 5 mins | 2025-10-29 01:27:33.915Z | 238.446° WSW | 2025-10-29 01:29:33.915Z | 182.438° SSW | 29.699° | 2025-10-29 01:32:33.915Z | 123.902° 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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