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 days ago
TLE from 6 days ago
0 YAOGAN-43 02C
1 60947U 24156C 25252.88057681 .00008066 00000-0 33376-3 0 9998
2 60947 34.9985 160.9834 0002610 345.4834 14.5805 15.23224211 56688Epoch: 2025-09-09T21:08Z
TLE epoch observation values (Epoch: 2025-09-09T21:08:01.836Z)
Latitude
-0.00004°
Longitude
-145.1893°
Altitude
493.294 km
Speed
7.621 km/s
True Right ascension
10h 43m 56s
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
05:46:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.169 km
Perigee altitude
497.579 km
Semi-major axis
6,877.511 km
Eccentricity
0.00026
Inclination
34.9985°
RAAN
160.9834°
Arg. of periapsis
345.4834°
True anomaly
14.58803°
Mean anomaly
14.5805°
Eccentric anomaly
14.58427°
Mean motion
3.80536 °/min
Orbital period
94.6 mins
BSTAR
0.00033376
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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 | 2025-09-15 20:35:18.216Z | 221.262° SW | 2025-09-15 20:37:18.216Z | 165.53° S | 29.306° | 2025-09-15 20:40:18.216Z | 107.697° ESE |
| 5 mins | 2025-09-15 22:14:18.216Z | 244.048° WSW | 2025-09-15 22:16:18.216Z | 198.235° SSW | 30.022° | 2025-09-15 22:19:18.216Z | 125.48° SE |
| 4 mins | 2025-09-15 23:54:18.216Z | 232.131° WSW | 2025-09-15 23:56:18.216Z | 193.286° SSW | 17.302° | 2025-09-15 23:58:18.216Z | 159.984° S |
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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