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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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 week ago
TLE from 1 week ago
0 YAOGAN-43 02E
1 60949U 24156E 26296.79894093 .00008064 00000-0 33265-3 0 9990
2 60949 34.9941 109.2894 0003898 27.0485 333.0432 15.23323507119063Epoch: 2026-10-23T19:10Z
TLE epoch observation values (Epoch: 2026-10-23T19:10:28.496Z)
Latitude
-0.00003°
Longitude
149.45632°
Altitude
492.343 km
Speed
7.622 km/s
True Right ascension
07h 17m 09s
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
21:44:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.757 km
Perigee altitude
496.395 km
Semi-major axis
6,877.213 km
Eccentricity
0.00039
Inclination
34.9941°
RAAN
109.2894°
Arg. of periapsis
27.0485°
True anomaly
333.02294°
Mean anomaly
333.0432°
Eccentric anomaly
333.03307°
Mean motion
3.80561 °/min
Orbital period
94.6 mins
BSTAR
0.00033265
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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 | 2026-11-03 11:51:13.118Z | 218.55° SW | 2026-11-03 11:53:13.118Z | 162.55° S | 33.413° | 2026-11-03 11:56:13.118Z | 106.688° ESE |
| 5 mins | 2026-11-03 13:30:13.118Z | 243.316° WSW | 2026-11-03 13:32:13.118Z | 195.03° SSW | 36.991° | 2026-11-03 13:35:13.118Z | 122.672° SE |
| 4 mins | 2026-11-03 15:10:13.118Z | 231.785° WSW | 2026-11-03 15:12:13.118Z | 190.575° SSW | 19.631° | 2026-11-03 15:14:13.118Z | 156.552° 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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