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: 13 hours ago
TLE from 13 hours ago
0 YAOGAN-43 02F
1 60950U 24156F 25357.10822598 .00009725 00000-0 40159-3 0 9990
2 60950 34.9917 225.3180 0001365 318.7532 41.3079 15.23259433 72583Epoch: 2025-12-23T02:35Z
TLE epoch observation values (Epoch: 2025-12-23T02:35:50.724Z)
Latitude
-0.00004°
Longitude
94.45988°
Altitude
494.218 km
Speed
7.62 km/s
True Right ascension
15h 01m 16s
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
14:59:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.208 km
Perigee altitude
498.33 km
Semi-major axis
6,877.406 km
Eccentricity
0.00014
Inclination
34.9917°
RAAN
225.318°
Arg. of periapsis
318.7532°
True anomaly
41.31823°
Mean anomaly
41.3079°
Eccentric anomaly
41.31306°
Mean motion
3.80545 °/min
Orbital period
94.6 mins
BSTAR
0.00040159
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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 | 2025-12-23 20:12:03.252Z | 209.953° SW | 2025-12-23 20:14:03.252Z | 154.417° SSE | 26.458° | 2025-12-23 20:16:03.252Z | 114.019° SE |
| 5 mins | 2025-12-23 21:51:03.252Z | 239.103° WSW | 2025-12-23 21:53:03.252Z | 184.39° SSW | 31.698° | 2025-12-23 21:56:03.252Z | 118.309° SE |
| 4 mins | 2025-12-23 23:31:03.252Z | 229.264° WSW | 2025-12-23 23:32:03.252Z | 208.06° SW | 20.619° | 2025-12-23 23:35:03.252Z | 150.186° 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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