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: 12 hours ago
TLE from 12 hours ago
0 YAOGAN-43 02C
1 60947U 24156C 25345.30880686 .00032545 00000-0 13479-2 0 9997
2 60947 34.9987 299.7147 0002612 120.2524 239.8450 15.22966079 70784Epoch: 2025-12-11T07:24Z
TLE epoch observation values (Epoch: 2025-12-11T07:24:40.912Z)
Latitude
0.00001°
Longitude
108.27761°
Altitude
496.709 km
Speed
7.618 km/s
True Right ascension
19h 58m 51s
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
18:16:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.947 km
Perigee altitude
498.353 km
Semi-major axis
6,878.287 km
Eccentricity
0.00026
Inclination
34.9987°
RAAN
299.7147°
Arg. of periapsis
120.2524°
True anomaly
239.81912°
Mean anomaly
239.845°
Eccentric anomaly
239.83206°
Mean motion
3.80472 °/min
Orbital period
94.62 mins
BSTAR
0.0013479
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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 | 2025-12-12 00:57:28.979Z | 202.728° SW | 2025-12-12 00:59:28.979Z | 167.984° S | 18.696° | 2025-12-12 01:02:28.979Z | 113.898° SE |
| 5 mins | 2025-12-12 02:37:28.979Z | 224.984° SW | 2025-12-12 02:39:28.979Z | 163.686° S | 30.701° | 2025-12-12 02:42:28.979Z | 108.229° ESE |
| 5 mins | 2025-12-12 04:16:28.979Z | 243.418° WSW | 2025-12-12 04:18:28.979Z | 196.992° SSW | 28.381° | 2025-12-12 04:21:28.979Z | 130.106° 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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