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 25261.01076323 .00019846 00000-0 69951-3 0 9991
2 60945 34.9969 105.9704 0003326 270.2197 89.8138 15.28390940 58016Epoch: 2025-09-18T00:15Z
TLE epoch observation values (Epoch: 2025-09-18T00:15:29.943Z)
Latitude
-0.00001°
Longitude
104.91713°
Altitude
479.519 km
Speed
7.628 km/s
True Right ascension
07h 03m 52s
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
21:36:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.163 km
Perigee altitude
481.598 km
Semi-major axis
6,862.017 km
Eccentricity
0.00033
Inclination
34.9969°
RAAN
105.9704°
Arg. of periapsis
270.2197°
True anomaly
89.85191°
Mean anomaly
89.8138°
Eccentric anomaly
89.83286°
Mean motion
3.81826 °/min
Orbital period
94.28 mins
BSTAR
0.00069951
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-18 17:45:23.618Z | 201.653° SSW | 2025-09-18 17:47:23.618Z | 161.706° S | 19.967° | 2025-09-18 17:49:23.618Z | 121.435° SE |
| 5 mins | 2025-09-18 19:24:23.618Z | 231.901° WSW | 2025-09-18 19:26:23.618Z | 177.683° S | 31.125° | 2025-09-18 19:29:23.618Z | 111.213° ESE |
| 5 mins | 2025-09-18 21:03:23.618Z | 242.7° WSW | 2025-09-18 21:05:23.618Z | 196.124° SSW | 26.959° | 2025-09-18 21:08:23.618Z | 132.254° 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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