YAOGAN-43 02D, 60948
Orbit data source: Space-Track
YAOGAN-43 02D, 60948 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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60948 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: 1 day ago
TLE from 1 day ago
0 YAOGAN-43 02D
1 60948U 24156D 25257.34563468 .00007535 00000-0 31278-3 0 9999
2 60948 34.9917 132.8591 0005122 284.8708 75.1440 15.23118599 57364Epoch: 2025-09-14T08:17Z
TLE epoch observation values (Epoch: 2025-09-14T08:17:42.836Z)
Latitude
0.00004°
Longitude
14.8647°
Altitude
494.446 km
Speed
7.62 km/s
True Right ascension
08h 51m 26s
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
03:54:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.215 km
Perigee altitude
496.17 km
Semi-major axis
6,877.829 km
Eccentricity
0.00051
Inclination
34.9917°
RAAN
132.8591°
Arg. of periapsis
284.8708°
True anomaly
75.20074°
Mean anomaly
75.144°
Eccentric anomaly
75.17237°
Mean motion
3.8051 °/min
Orbital period
94.61 mins
BSTAR
0.00031278
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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 02D 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 | 2025-09-15 19:08:23.031Z | 199.351° SSW | 2025-09-15 19:10:23.031Z | 165.057° S | 17.713° | 2025-09-15 19:13:23.031Z | 113.589° SE |
| 5 mins | 2025-09-15 20:48:23.031Z | 221.398° SW | 2025-09-15 20:50:23.031Z | 159.324° S | 30.06° | 2025-09-15 20:53:23.031Z | 107.112° ESE |
| 5 mins | 2025-09-15 22:27:23.031Z | 242.083° WSW | 2025-09-15 22:29:23.031Z | 192.733° SSW | 29.369° | 2025-09-15 22:32:23.031Z | 127.306° 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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