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: 12 hours ago
TLE from 12 hours ago
0 YAOGAN-43 02E
1 60949U 24156E 25310.04911162 .00018122 00000-0 75008-3 0 9998
2 60949 34.9952 161.4874 0006049 227.7890 132.2311 15.23068060 65406Epoch: 2025-11-06T01:10Z
TLE epoch observation values (Epoch: 2025-11-06T01:10:43.243Z)
Latitude
-0.00007°
Longitude
98.29412°
Altitude
498.295 km
Speed
7.616 km/s
True Right ascension
10h 45m 56s
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
09:16:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.004 km
Perigee altitude
495.683 km
Semi-major axis
6,877.981 km
Eccentricity
0.0006
Inclination
34.9952°
RAAN
161.4874°
Arg. of periapsis
227.789°
True anomaly
132.2824°
Mean anomaly
132.2311°
Eccentric anomaly
132.25675°
Mean motion
3.80497 °/min
Orbital period
94.61 mins
BSTAR
0.00075008
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-06 18:46:04.066Z | 208.645° SW | 2025-11-06 18:48:04.066Z | 159.832° S | 25.053° | 2025-11-06 18:51:04.066Z | 106.975° ESE |
| 5 mins | 2025-11-06 20:25:04.066Z | 239.958° WSW | 2025-11-06 20:27:04.066Z | 191.384° SSW | 31.918° | 2025-11-06 20:30:04.066Z | 117.127° SE |
| 4 mins | 2025-11-06 22:05:04.066Z | 234.581° WSW | 2025-11-06 22:07:04.066Z | 187.245° SSW | 23.103° | 2025-11-06 22:09:04.066Z | 148.107° 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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