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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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: 19 hours ago
TLE from 19 hours ago
0 YAOGAN-43 02C
1 60947U 24156C 26040.09034817 .00008573 00000-0 35655-3 0 9998
2 60947 34.9974 283.7313 0006191 300.6351 59.3753 15.23026416 79903Epoch: 2026-02-09T02:10Z
TLE epoch observation values (Epoch: 2026-02-09T02:10:06.081Z)
Latitude
-0.00003°
Longitude
112.01576°
Altitude
493.459 km
Speed
7.622 km/s
True Right ascension
18h 54m 55s
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
23:41:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.227 km
Perigee altitude
495.71 km
Semi-major axis
6,878.106 km
Eccentricity
0.00062
Inclination
34.9974°
RAAN
283.7313°
Arg. of periapsis
300.6351°
True anomaly
59.43637°
Mean anomaly
59.3753°
Eccentric anomaly
59.40583°
Mean motion
3.80487 °/min
Orbital period
94.62 mins
BSTAR
0.00035655
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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 | 2026-02-09 21:21:42.190Z | 226.408° WSW | 2026-02-09 21:23:42.190Z | 176.286° S | 29.972° | 2026-02-09 21:26:42.190Z | 110.009° ESE |
| 5 mins | 2026-02-09 23:01:42.190Z | 234.098° WSW | 2026-02-09 23:03:42.190Z | 172.516° S | 29.52° | 2026-02-09 23:06:42.190Z | 121.533° SE |
| 5 mins | 2026-02-10 20:57:42.190Z | 229.011° WSW | 2026-02-10 20:59:42.190Z | 181.215° SSW | 30.188° | 2026-02-10 21:02:42.190Z | 111.14° ESE |
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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