YAOGAN-43 02F, 60950
Orbit data source: Space-Track
YAOGAN-43 02F, 60950 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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60950 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: 2 weeks ago
TLE from 2 weeks ago
0 YAOGAN-43 02F
1 60950U 24156F 25244.35986002 .00015484 00000-0 63843-3 0 9997
2 60950 34.9915 214.4382 0001154 236.1390 123.9215 15.23236528 55383Epoch: 2025-09-01T08:38Z
TLE epoch observation values (Epoch: 2025-09-01T08:38:11.905Z)
Latitude
-0.00002°
Longitude
104.122°
Altitude
495.435 km
Speed
7.619 km/s
True Right ascension
14h 17m 45s
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
05:50:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.131 km
Perigee altitude
498.544 km
Semi-major axis
6,877.475 km
Eccentricity
0.00012
Inclination
34.9915°
RAAN
214.4382°
Arg. of periapsis
236.139°
True anomaly
123.93247°
Mean anomaly
123.9215°
Eccentric anomaly
123.92699°
Mean motion
3.80539 °/min
Orbital period
94.6 mins
BSTAR
0.00063843
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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 02F 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 | 2025-09-15 18:52:38.194Z | 187.639° SSW | 2025-09-15 18:54:38.194Z | 152.646° SSE | 15.254° | 2025-09-15 18:56:38.194Z | 120.125° SE |
| 5 mins | 2025-09-15 20:31:38.194Z | 223.283° SW | 2025-09-15 20:33:38.194Z | 172.36° S | 29.118° | 2025-09-15 20:36:38.194Z | 109.114° ESE |
| 5 mins | 2025-09-15 22:10:38.194Z | 245.718° WSW | 2025-09-15 22:12:38.194Z | 204.26° SW | 29.643° | 2025-09-15 22:15:38.194Z | 126.433° 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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