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: 12 hours ago
TLE from 12 hours ago
0 YAOGAN-43 02B
1 60946U 24156B 25341.96996330 .00018406 00000-0 76402-3 0 9994
2 60946 34.9957 320.6533 0008979 181.3626 178.7065 15.22949241 70275Epoch: 2025-12-07T23:16Z
TLE epoch observation values (Epoch: 2025-12-07T23:16:44.829Z)
Latitude
-0.00001°
Longitude
-105.50922°
Altitude
502.027 km
Speed
7.612 km/s
True Right ascension
21h 22m 36s
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
09:18:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.377 km
Perigee altitude
494.025 km
Semi-major axis
6,878.338 km
Eccentricity
0.0009
Inclination
34.9957°
RAAN
320.6533°
Arg. of periapsis
181.3626°
True anomaly
178.70882°
Mean anomaly
178.7065°
Eccentric anomaly
178.70766°
Mean motion
3.80468 °/min
Orbital period
94.62 mins
BSTAR
0.00076402
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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 | 2025-12-09 02:16:11.978Z | 192.393° SSW | 2025-12-09 02:18:11.978Z | 154.154° SSE | 17.89° | 2025-12-09 02:20:11.978Z | 119.234° SE |
| 5 mins | 2025-12-09 03:55:11.978Z | 228.849° WSW | 2025-12-09 03:57:11.978Z | 178.436° S | 30.584° | 2025-12-09 04:00:11.978Z | 110.608° ESE |
| 5 mins | 2025-12-09 05:35:11.978Z | 234.58° WSW | 2025-12-09 05:37:11.978Z | 174.934° S | 28.737° | 2025-12-09 05:40:11.978Z | 123.706° 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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