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: 16 hours ago
TLE from 16 hours ago
0 YAOGAN-43 02B
1 60946U 24156B 26126.36135631 .00009277 00000-0 38537-3 0 9992
2 60946 34.9935 101.0818 0001806 173.7450 186.3288 15.23066840 93060Epoch: 2026-05-06T08:40Z
TLE epoch observation values (Epoch: 2026-05-06T08:40:21.185Z)
Latitude
0.00003°
Longitude
106.77062°
Altitude
496.737 km
Speed
7.618 km/s
True Right ascension
06h 44m 19s
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
09:09:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.09 km
Perigee altitude
498.606 km
Semi-major axis
6,877.985 km
Eccentricity
0.00018
Inclination
34.9935°
RAAN
101.0818°
Arg. of periapsis
173.745°
True anomaly
186.32652°
Mean anomaly
186.3288°
Eccentric anomaly
186.32766°
Mean motion
3.80497 °/min
Orbital period
94.61 mins
BSTAR
0.00038537
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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 | 2026-05-07 02:13:20.727Z | 205.42° SW | 2026-05-07 02:15:20.727Z | 170.417° S | 19.578° | 2026-05-07 02:18:20.727Z | 114.187° SE |
| 5 mins | 2026-05-07 03:53:20.727Z | 227.501° WSW | 2026-05-07 03:55:20.727Z | 167.128° S | 31.205° | 2026-05-07 03:58:20.727Z | 109.245° ESE |
| 5 mins | 2026-05-07 05:32:20.727Z | 244.135° WSW | 2026-05-07 05:34:20.727Z | 199.727° SSW | 27.634° | 2026-05-07 05:37:20.727Z | 132.48° 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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