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: 3 days ago
TLE from 3 days ago
0 YAOGAN-43 02D
1 60948U 24156D 26033.80362782 .00012410 00000-0 51117-3 0 9991
2 60948 34.9938 323.1413 0003861 130.7325 229.3726 15.23298968 78943Epoch: 2026-02-02T19:17Z
TLE epoch observation values (Epoch: 2026-02-02T19:17:13.443Z)
Latitude
0.00002°
Longitude
-99.15836°
Altitude
496.533 km
Speed
7.618 km/s
True Right ascension
21h 32m 33s
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
04:05:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.805 km
Perigee altitude
496.494 km
Semi-major axis
6,877.287 km
Eccentricity
0.00039
Inclination
34.9938°
RAAN
323.1413°
Arg. of periapsis
130.7325°
True anomaly
229.33903°
Mean anomaly
229.3726°
Eccentric anomaly
229.35581°
Mean motion
3.80555 °/min
Orbital period
94.6 mins
BSTAR
0.00051117
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-06 02:24:41.064Z | 234.481° WSW | 2026-02-06 02:26:41.064Z | 195.403° SSW | 18.085° | 2026-02-06 02:28:41.064Z | 160.153° S |
| 5 mins | 2026-02-06 22:41:41.064Z | 219.738° SW | 2026-02-06 22:43:41.064Z | 162.351° S | 29.148° | 2026-02-06 22:46:41.064Z | 107.097° ESE |
| 5 mins | 2026-02-07 00:20:41.064Z | 242.943° WSW | 2026-02-07 00:22:41.064Z | 194.729° SSW | 30.225° | 2026-02-07 00:25:41.064Z | 124.599° 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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