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: 10 hours ago
TLE from 10 hours ago
0 YAOGAN-43 02B
1 60946U 24156B 26068.41368763 .00015184 00000-0 62308-3 0 9994
2 60946 34.9944 105.5294 0002154 182.9946 177.0756 15.23399653 84222Epoch: 2026-03-09T09:55Z
TLE epoch observation values (Epoch: 2026-03-09T09:55:42.611Z)
Latitude
-0.00001°
Longitude
149.49486°
Altitude
495.98 km
Speed
7.618 km/s
True Right ascension
07h 02m 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
00:31:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.328 km
Perigee altitude
497.365 km
Semi-major axis
6,876.984 km
Eccentricity
0.00022
Inclination
34.9944°
RAAN
105.5294°
Arg. of periapsis
182.9946°
True anomaly
177.07686°
Mean anomaly
177.0756°
Eccentric anomaly
177.07623°
Mean motion
3.8058 °/min
Orbital period
94.59 mins
BSTAR
0.00062308
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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 | 2026-03-10 06:38:13.362Z | 213.658° SW | 2026-03-10 06:40:13.362Z | 176.908° S | 22.628° | 2026-03-10 06:43:13.362Z | 113.875° SE |
| 5 mins | 2026-03-10 08:18:13.362Z | 233.414° WSW | 2026-03-10 08:20:13.362Z | 174.177° S | 32.012° | 2026-03-10 08:23:13.362Z | 112.457° ESE |
| 4 mins | 2026-03-10 09:58:13.362Z | 228.311° WSW | 2026-03-10 09:59:13.362Z | 203.259° SW | 24.791° | 2026-03-10 10:02:13.362Z | 139.739° 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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