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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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: 7 hours ago
TLE from 7 hours ago
0 YAOGAN-43 02F
1 60950U 24156F 26256.73919704 .00006688 00000-0 27919-3 0 9998
2 60950 34.9946 0.9382 0001263 34.6161 325.4636 15.22965953112956Epoch: 2026-09-13T17:44Z
TLE epoch observation values (Epoch: 2026-09-13T17:44:26.624Z)
Latitude
0.00001°
Longitude
102.09776°
Altitude
495.092 km
Speed
7.62 km/s
True Right ascension
00h 03m 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
16:54:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.02 km
Perigee altitude
499.282 km
Semi-major axis
6,878.288 km
Eccentricity
0.00013
Inclination
34.9946°
RAAN
0.9382°
Arg. of periapsis
34.6161°
True anomaly
325.45539°
Mean anomaly
325.4636°
Eccentric anomaly
325.4595°
Mean motion
3.80472 °/min
Orbital period
94.62 mins
BSTAR
0.00027919
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-14 11:18:19.231Z | 213.638° SW | 2026-09-14 11:21:19.231Z | 151.251° SSE | 24.647° | 2026-09-14 11:23:19.231Z | 114.272° SE |
| 5 mins | 2026-09-14 12:58:19.231Z | 234.554° WSW | 2026-09-14 13:00:19.231Z | 177.209° S | 39.519° | 2026-09-14 13:03:19.231Z | 112.254° ESE |
| 4 mins | 2026-09-14 14:38:19.231Z | 231.145° WSW | 2026-09-14 14:39:19.231Z | 206.733° SW | 28.224° | 2026-09-14 14:42:19.231Z | 139.806° 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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