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: 21 hours ago
TLE from 21 hours ago
0 YAOGAN-43 02C
1 60947U 24156C 25314.95732106 .00016268 00000-0 67544-3 0 9994
2 60947 34.9975 130.5732 0001847 194.7157 165.3504 15.22995066 66157Epoch: 2025-11-10T22:58Z
TLE epoch observation values (Epoch: 2025-11-10T22:58:32.539Z)
Latitude
-0.00002°
Longitude
95.58681°
Altitude
496.948 km
Speed
7.618 km/s
True Right ascension
08h 42m 17s
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
16:50:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.333 km
Perigee altitude
498.793 km
Semi-major axis
6,878.2 km
Eccentricity
0.00018
Inclination
34.9975°
RAAN
130.5732°
Arg. of periapsis
194.7157°
True anomaly
165.35575°
Mean anomaly
165.3504°
Eccentric anomaly
165.35308°
Mean motion
3.80479 °/min
Orbital period
94.62 mins
BSTAR
0.00067544
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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 | 2025-11-12 16:10:50.324Z | 209.955° SW | 2025-11-12 16:12:50.324Z | 154.305° SSE | 26.529° | 2025-11-12 16:14:50.324Z | 113.957° SE |
| 5 mins | 2025-11-12 17:49:50.324Z | 239.306° WSW | 2025-11-12 17:51:50.324Z | 184.926° SSW | 31.728° | 2025-11-12 17:54:50.324Z | 118.414° SE |
| 4 mins | 2025-11-12 19:29:50.324Z | 229.75° WSW | 2025-11-12 19:30:50.324Z | 208.711° SW | 20.563° | 2025-11-12 19:33:50.324Z | 150.531° SSE |
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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