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: 21 hours ago
TLE from 21 hours ago
0 YAOGAN-43 02F
1 60950U 24156F 26040.09180084 .00010106 00000-0 42067-3 0 9990
2 60950 34.9919 283.5296 0001521 290.7699 69.2852 15.22983320 79905Epoch: 2026-02-09T02:12Z
TLE epoch observation values (Epoch: 2026-02-09T02:12:11.592Z)
Latitude
-0.00005°
Longitude
111.28964°
Altitude
495.384 km
Speed
7.62 km/s
True Right ascension
18h 54m 07s
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
01:43:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.145 km
Perigee altitude
499.053 km
Semi-major axis
6,878.236 km
Eccentricity
0.00015
Inclination
34.9919°
RAAN
283.5296°
Arg. of periapsis
290.7699°
True anomaly
69.3015°
Mean anomaly
69.2852°
Eccentric anomaly
69.29335°
Mean motion
3.80476 °/min
Orbital period
94.62 mins
BSTAR
0.00042067
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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 | 2026-02-10 00:43:06.119Z | 234.423° WSW | 2026-02-10 00:45:06.119Z | 198.246° SSW | 16.301° | 2026-02-10 00:47:06.119Z | 164.779° S |
| 5 mins | 2026-02-10 21:00:06.119Z | 228.792° WSW | 2026-02-10 21:02:06.119Z | 178.613° S | 30.473° | 2026-02-10 21:05:06.119Z | 110.642° ESE |
| 5 mins | 2026-02-10 22:40:06.119Z | 234.64° WSW | 2026-02-10 22:42:06.119Z | 174.995° S | 28.819° | 2026-02-10 22:45:06.119Z | 123.618° 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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