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: 6 hours ago
TLE from 6 hours ago
0 YAOGAN-43 02A
1 60945U 24156A 26131.17574914 .00030410 00000-0 59168-3 0 9993
2 60945 34.9961 34.5447 0005238 294.0169 66.0005 15.46568440 94221Epoch: 2026-05-11T04:13Z
TLE epoch observation values (Epoch: 2026-05-11T04:13:04.725Z)
Latitude
0°
Longitude
102.30678°
Altitude
424.221 km
Speed
7.66 km/s
True Right ascension
02h 18m 10s
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
18:10:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
433.624 km
Perigee altitude
426.491 km
Semi-major axis
6,808.195 km
Eccentricity
0.00052
Inclination
34.9961°
RAAN
34.5447°
Arg. of periapsis
294.0169°
True anomaly
66.05535°
Mean anomaly
66.0005°
Eccentric anomaly
66.02792°
Mean motion
3.86363 °/min
Orbital period
93.18 mins
BSTAR
0.00059168
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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 | 2026-05-11 21:30:48.031Z | 196.769° SSW | 2026-05-11 21:32:48.031Z | 154.006° SSE | 17.466° | 2026-05-11 21:34:48.031Z | 117.023° SE |
| 4 mins | 2026-05-11 23:08:48.031Z | 223.033° SW | 2026-05-11 23:09:48.031Z | 195.51° SSW | 27.873° | 2026-05-11 23:12:48.031Z | 114.522° SE |
| 4 mins | 2026-05-12 00:46:48.031Z | 230.562° WSW | 2026-05-12 00:47:48.031Z | 203.636° SW | 24.933° | 2026-05-12 00:50:48.031Z | 132.919° 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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