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 25289.26910890 .00011923 00000-0 49362-3 0 9999
2 60948 34.9934 292.0795 0006168 223.9846 136.0378 15.23123896 62231Epoch: 2025-10-16T06:27Z
TLE epoch observation values (Epoch: 2025-10-16T06:27:31.008Z)
Latitude
-0.00004°
Longitude
170.16898°
Altitude
498.384 km
Speed
7.616 km/s
True Right ascension
19h 28m 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
07:01:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.918 km
Perigee altitude
495.434 km
Semi-major axis
6,877.813 km
Eccentricity
0.00062
Inclination
34.9934°
RAAN
292.0795°
Arg. of periapsis
223.9846°
True anomaly
136.08684°
Mean anomaly
136.0378°
Eccentric anomaly
136.06232°
Mean motion
3.80511 °/min
Orbital period
94.61 mins
BSTAR
0.00049362
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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 | 2025-10-18 04:22:03.824Z | 210.384° SW | 2025-10-18 04:24:03.824Z | 160.087° S | 25.819° | 2025-10-18 04:27:03.824Z | 106.818° ESE |
| 5 mins | 2025-10-18 06:01:03.824Z | 240.617° WSW | 2025-10-18 06:03:03.824Z | 191.853° SSW | 31.841° | 2025-10-18 06:06:03.824Z | 118.098° SE |
| 4 mins | 2025-10-18 07:41:03.824Z | 233.899° WSW | 2025-10-18 07:43:03.824Z | 187.783° SSW | 22.214° | 2025-10-18 07:45:03.824Z | 149.783° 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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