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: 17 hours ago
TLE from 17 hours ago
0 YAOGAN-43 02F
1 60950U 24156F 25309.97619931 .00012266 00000-0 51123-3 0 9994
2 60950 34.9886 161.7456 0002750 345.3072 14.7562 15.22907694 65391Epoch: 2025-11-05T23:25Z
TLE epoch observation values (Epoch: 2025-11-05T23:25:43.620Z)
Latitude
-0.00002°
Longitude
124.87267°
Altitude
494.153 km
Speed
7.621 km/s
True Right ascension
10h 46m 58s
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
12:28:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.219 km
Perigee altitude
498.436 km
Semi-major axis
6,878.464 km
Eccentricity
0.00028
Inclination
34.9886°
RAAN
161.7456°
Arg. of periapsis
345.3072°
True anomaly
14.76423°
Mean anomaly
14.7562°
Eccentric anomaly
14.76021°
Mean motion
3.80457 °/min
Orbital period
94.62 mins
BSTAR
0.00051123
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-06 18:33:39.830Z | 221.321° SW | 2025-11-06 18:36:39.830Z | 169.461° S | 23.48° | 2025-11-06 18:39:39.830Z | 110.661° ESE |
| 5 mins | 2025-11-06 20:14:39.830Z | 229.726° WSW | 2025-11-06 20:16:39.830Z | 163.859° S | 31.471° | 2025-11-06 20:19:39.830Z | 111.253° ESE |
| 5 mins | 2025-11-06 21:53:39.830Z | 241.143° WSW | 2025-11-06 21:55:39.830Z | 196.851° SSW | 24.738° | 2025-11-06 21:58:39.830Z | 138.437° 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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