YAOGAN-43 02B, 60946
Orbit data source: Space-Track
YAOGAN-43 02B, 60946 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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60946 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: 4 days ago
TLE from 4 days ago
0 YAOGAN-43 02B
1 60946U 24156B 25254.39099109 .00017963 00000-0 73484-3 0 9996
2 60946 34.9942 151.4265 0004111 221.0696 138.9710 15.23472567 56917Epoch: 2025-09-11T09:23Z
TLE epoch observation values (Epoch: 2025-09-11T09:23:01.63Z)
Latitude
0.00002°
Longitude
20.01601°
Altitude
496.414 km
Speed
7.618 km/s
True Right ascension
10h 05m 42s
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
05:46:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.455 km
Perigee altitude
495.801 km
Semi-major axis
6,876.765 km
Eccentricity
0.00041
Inclination
34.9942°
RAAN
151.4265°
Arg. of periapsis
221.0696°
True anomaly
139.00191°
Mean anomaly
138.971°
Eccentric anomaly
138.98646°
Mean motion
3.80598 °/min
Orbital period
94.59 mins
BSTAR
0.00073484
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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 02B 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 18:59:19.221Z | 190.556° SSW | 2025-09-15 19:01:19.221Z | 154.727° SSE | 16.357° | 2025-09-15 19:03:19.221Z | 120.733° SE |
| 5 mins | 2025-09-15 20:38:19.221Z | 226.356° WSW | 2025-09-15 20:40:19.221Z | 177.032° S | 29.755° | 2025-09-15 20:43:19.221Z | 110.165° ESE |
| 5 mins | 2025-09-15 22:18:19.221Z | 233.786° WSW | 2025-09-15 22:20:19.221Z | 171.658° S | 29.474° | 2025-09-15 22:23:19.221Z | 121.082° 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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