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: 11 hours ago
TLE from 11 hours ago
0 YAOGAN-43 02A
1 60945U 24156A 25258.07124124 .00019381 00000-0 68586-3 0 9993
2 60945 34.9963 124.6080 0003224 251.2885 108.7481 15.28262765 57569Epoch: 2025-09-15T01:42Z
TLE epoch observation values (Epoch: 2025-09-15T01:42:35.243Z)
Latitude
-0.00003°
Longitude
104.67995°
Altitude
480.621 km
Speed
7.627 km/s
True Right ascension
08h 18m 25s
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
486.476 km
Perigee altitude
482.051 km
Semi-major axis
6,862.401 km
Eccentricity
0.00032
Inclination
34.9963°
RAAN
124.608°
Arg. of periapsis
251.2885°
True anomaly
108.78308°
Mean anomaly
108.7481°
Eccentric anomaly
108.76559°
Mean motion
3.81794 °/min
Orbital period
94.29 mins
BSTAR
0.00068586
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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 | 2025-09-15 19:12:17.707Z | 206.343° SW | 2025-09-15 19:14:17.707Z | 169.809° S | 19.916° | 2025-09-15 19:17:17.707Z | 113.054° SE |
| 5 mins | 2025-09-15 20:51:17.707Z | 236.105° WSW | 2025-09-15 20:53:17.707Z | 191.661° SSW | 30.526° | 2025-09-15 20:56:17.707Z | 114.099° SE |
| 4 mins | 2025-09-15 22:31:17.707Z | 232.389° WSW | 2025-09-15 22:32:17.707Z | 207.452° SW | 26.098° | 2025-09-15 22:35:17.707Z | 135.974° SSE |
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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