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: 8 hours ago
TLE from 8 hours ago
0 YAOGAN-43 02C
1 60947U 24156C 26130.55177722 .00004557 00000-0 18986-3 0 9998
2 60947 34.9978 74.8185 0003758 16.7053 343.3785 15.23129269 93708Epoch: 2026-05-10T13:14Z
TLE epoch observation values (Epoch: 2026-05-10T13:14:33.551Z)
Latitude
-0.00003°
Longitude
7.82544°
Altitude
492.841 km
Speed
7.622 km/s
True Right ascension
04h 59m 16s
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
05:35:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.244 km
Perigee altitude
497.075 km
Semi-major axis
6,877.796 km
Eccentricity
0.00038
Inclination
34.9978°
RAAN
74.8185°
Arg. of periapsis
16.7053°
True anomaly
343.36618°
Mean anomaly
343.3785°
Eccentric anomaly
343.37234°
Mean motion
3.80513 °/min
Orbital period
94.61 mins
BSTAR
0.00018986
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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 | 2026-05-11 00:30:41.806Z | 206.447° SW | 2026-05-11 00:32:41.806Z | 167.395° S | 21.381° | 2026-05-11 00:35:41.806Z | 111.333° ESE |
| 5 mins | 2026-05-11 02:10:41.806Z | 226.705° WSW | 2026-05-11 02:12:41.806Z | 160.788° S | 31.082° | 2026-05-11 02:15:41.806Z | 109.194° ESE |
| 5 mins | 2026-05-11 03:49:41.806Z | 241.279° WSW | 2026-05-11 03:51:41.806Z | 194.188° SSW | 26.562° | 2026-05-11 03:54:41.806Z | 133.839° 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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