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: 18 hours ago
TLE from 18 hours ago
0 YAOGAN-43 02E
1 60949U 24156E 25261.01885293 .00015167 00000-0 62929-3 0 9999
2 60949 34.9954 109.8783 0001079 260.1746 99.8846 15.23030431 57922Epoch: 2025-09-18T00:27Z
TLE epoch observation values (Epoch: 2025-09-18T00:27:08.893Z)
Latitude
-0.00005°
Longitude
105.90471°
Altitude
495.74 km
Speed
7.619 km/s
True Right ascension
07h 19m 30s
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
11:19:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.699 km
Perigee altitude
499.215 km
Semi-major axis
6,878.094 km
Eccentricity
0.00011
Inclination
34.9954°
RAAN
109.8783°
Arg. of periapsis
260.1746°
True anomaly
99.89678°
Mean anomaly
99.8846°
Eccentric anomaly
99.89069°
Mean motion
3.80488 °/min
Orbital period
94.62 mins
BSTAR
0.00062929
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-18 19:39:20.492Z | 239.646° WSW | 2025-09-18 19:42:20.492Z | 167.835° S | 31.414° | 2025-09-18 19:45:20.492Z | 109.635° ESE |
| 5 mins | 2025-09-18 21:19:20.492Z | 244.18° WSW | 2025-09-18 21:21:20.492Z | 200.281° SSW | 27.255° | 2025-09-18 21:24:20.492Z | 133.608° SE |
| 4 mins | 2025-09-19 17:37:20.492Z | 194.744° SSW | 2025-09-19 17:38:20.492Z | 173.946° S | 20.663° | 2025-09-19 17:41:20.492Z | 114.616° 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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