YAOGAN-43 02E, 60949
Orbit data source: Space-Track
YAOGAN-43 02E, 60949 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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60949 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: 2 days ago
TLE from 2 days ago
0 YAOGAN-43 02E
1 60949U 24156E 26039.11829322 .00006078 00000-0 25214-3 0 9992
2 60949 34.9948 289.9193 0007248 246.1175 113.8781 15.23177703 79758Epoch: 2026-02-08T02:50Z
TLE epoch observation values (Epoch: 2026-02-08T02:50:20.534Z)
Latitude
0.00003°
Longitude
109.10173°
Altitude
497.189 km
Speed
7.617 km/s
True Right ascension
19h 19m 40s
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
01:43:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.499 km
Perigee altitude
494.529 km
Semi-major axis
6,877.651 km
Eccentricity
0.00072
Inclination
34.9948°
RAAN
289.9193°
Arg. of periapsis
246.1175°
True anomaly
113.95402°
Mean anomaly
113.8781°
Eccentric anomaly
113.91606°
Mean motion
3.80525 °/min
Orbital period
94.61 mins
BSTAR
0.00025214
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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 02E 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 | 2026-02-10 00:57:05.165Z | 239.185° WSW | 2026-02-10 00:59:05.165Z | 207.667° SW | 14.379° | 2026-02-10 01:01:05.165Z | 174.219° S |
| 5 mins | 2026-02-10 21:14:05.165Z | 235.043° WSW | 2026-02-10 21:16:05.165Z | 191.42° SSW | 30.795° | 2026-02-10 21:19:05.165Z | 113.927° SE |
| 5 mins | 2026-02-10 22:54:05.165Z | 238.796° WSW | 2026-02-10 22:56:05.165Z | 186.393° SSW | 28.068° | 2026-02-10 22:59:05.165Z | 129.003° 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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