YAOGAN-43 02A, 60945
Orbit data source: Space-Track
YAOGAN-43 02A, 60945 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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60945 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 YAOGAN-43 02A
1 60945U 24156A 25346.21437530 .00045551 00000-0 13130-2 0 9997
2 60945 34.9964 283.1723 0006113 288.2822 71.7231 15.34659849 71081Epoch: 2025-12-12T05:08Z
TLE epoch observation values (Epoch: 2025-12-12T05:08:42.025Z)
Latitude
-0.00003°
Longitude
124.83794°
Altitude
459.523 km
Speed
7.64 km/s
True Right ascension
18h 52m 41s
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
08:44:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
469.382 km
Perigee altitude
461.015 km
Semi-major axis
6,843.335 km
Eccentricity
0.00061
Inclination
34.9964°
RAAN
283.1723°
Arg. of periapsis
288.2822°
True anomaly
71.78963°
Mean anomaly
71.7231°
Eccentric anomaly
71.75636°
Mean motion
3.83391 °/min
Orbital period
93.9 mins
BSTAR
0.001313
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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 02A 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 | 2025-12-13 00:07:50.335Z | 214.272° SW | 2025-12-13 00:10:50.335Z | 155.476° SSE | 20.913° | 2025-12-13 00:12:50.335Z | 116.614° SE |
| 5 mins | 2025-12-13 01:46:50.335Z | 237.834° WSW | 2025-12-13 01:48:50.335Z | 191.751° SSW | 30.415° | 2025-12-13 01:51:50.335Z | 114.752° SE |
| 5 mins | 2025-12-13 03:25:50.335Z | 240.586° WSW | 2025-12-13 03:27:50.335Z | 192.946° SSW | 24.985° | 2025-12-13 03:30:50.335Z | 134.278° 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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