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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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 26126.85046825 .00036453 00000-0 71537-3 0 9994
2 60945 34.9960 62.7345 0005232 264.9953 95.0172 15.46290008 93555Epoch: 2026-05-06T20:24Z
TLE epoch observation values (Epoch: 2026-05-06T20:24:40.456Z)
Latitude
-0.00001°
Longitude
-108.13912°
Altitude
426.799 km
Speed
7.658 km/s
True Right ascension
04h 10m 56s
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
09:07:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
434.437 km
Perigee altitude
427.312 km
Semi-major axis
6,809.011 km
Eccentricity
0.00052
Inclination
34.996°
RAAN
62.7345°
Arg. of periapsis
264.9953°
True anomaly
95.07692°
Mean anomaly
95.0172°
Eccentric anomaly
95.04706°
Mean motion
3.86293 °/min
Orbital period
93.19 mins
BSTAR
0.00071537
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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 | 2026-05-07 01:22:37.271Z | 229.865° WSW | 2026-05-07 01:24:37.271Z | 179.426° S | 28.224° | 2026-05-07 01:27:37.271Z | 110.476° ESE |
| 5 mins | 2026-05-07 03:00:37.271Z | 241.813° WSW | 2026-05-07 03:02:37.271Z | 190.775° SSW | 26.856° | 2026-05-07 03:05:37.271Z | 126.502° SE |
| 4 mins | 2026-05-08 00:36:37.271Z | 220.266° SW | 2026-05-08 00:38:37.271Z | 163.432° S | 26.625° | 2026-05-08 00:40:37.271Z | 116.19° 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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