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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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: 9 hours ago
TLE from 9 hours ago
0 YAOGAN-43 02B
1 60946U 24156B 26306.69248271 .00007008 00000-0 29171-3 0 9997
2 60946 34.9959 46.9171 0002724 303.4938 56.5516 15.23052116120578Epoch: 2026-11-02T16:37Z
TLE epoch observation values (Epoch: 2026-11-02T16:37:10.506Z)
Latitude
-0.00001°
Longitude
115.65746°
Altitude
494.516 km
Speed
7.62 km/s
True Right ascension
03h 07m 40s
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
21:44:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.765 km
Perigee altitude
498.018 km
Semi-major axis
6,878.029 km
Eccentricity
0.00027
Inclination
34.9959°
RAAN
46.9171°
Arg. of periapsis
303.4938°
True anomaly
56.57765°
Mean anomaly
56.5516°
Eccentric anomaly
56.56462°
Mean motion
3.80493 °/min
Orbital period
94.61 mins
BSTAR
0.00029171
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-03 11:48:13.129Z | 219.223° SW | 2026-11-03 11:50:13.129Z | 165.583° S | 33.427° | 2026-11-03 11:53:13.129Z | 107.327° ESE |
| 5 mins | 2026-11-03 13:27:13.129Z | 244.538° WSW | 2026-11-03 13:29:13.129Z | 199.725° SSW | 36.967° | 2026-11-03 13:32:13.129Z | 123.234° SE |
| 4 mins | 2026-11-03 15:07:13.129Z | 234.557° WSW | 2026-11-03 15:09:13.129Z | 193.896° SSW | 20.559° | 2026-11-03 15:11:13.129Z | 157.867° S |
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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