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: 6 hours ago
TLE from 6 hours ago
0 YAOGAN-43 02C
1 60947U 24156C 26036.81274543 .00014378 00000-0 59752-3 0 9999
2 60947 34.9986 304.3431 0006311 275.2672 84.7323 15.22965439 79400Epoch: 2026-02-05T19:30Z
TLE epoch observation values (Epoch: 2026-02-05T19:30:21.205Z)
Latitude
0.00003°
Longitude
-124.20481°
Altitude
495.413 km
Speed
7.62 km/s
True Right ascension
20h 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
04:04:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.493 km
Perigee altitude
495.811 km
Semi-major axis
6,878.289 km
Eccentricity
0.00063
Inclination
34.9986°
RAAN
304.3431°
Arg. of periapsis
275.2672°
True anomaly
84.80432°
Mean anomaly
84.7323°
Eccentric anomaly
84.76831°
Mean motion
3.80472 °/min
Orbital period
94.62 mins
BSTAR
0.00059752
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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 | 2026-02-06 02:15:08.672Z | 249.384° W | 2026-02-06 02:18:08.672Z | 197.973° SSW | 19.812° | 2026-02-06 02:20:08.672Z | 159.61° S |
| 5 mins | 2026-02-06 22:33:08.672Z | 223.969° SW | 2026-02-06 22:35:08.672Z | 178.283° S | 28.514° | 2026-02-06 22:38:08.672Z | 110.654° ESE |
| 5 mins | 2026-02-07 00:13:08.672Z | 235.683° WSW | 2026-02-07 00:15:08.672Z | 174.366° S | 30.876° | 2026-02-07 00:18:08.672Z | 119.042° 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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