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: 4 days ago
TLE from 4 days ago
0 YAOGAN-43 02E
1 60949U 24156E 25353.77279961 -.00000135 00000-0 -40798-5 0 9996
2 60949 34.9956 246.5175 0005458 195.3524 164.7026 15.22798785 72073Epoch: 2025-12-19T18:32Z
TLE epoch observation values (Epoch: 2025-12-19T18:32:49.886Z)
Latitude
0.00002°
Longitude
-120.29948°
Altitude
499.929 km
Speed
7.615 km/s
True Right ascension
16h 26m 04s
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
12:42:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.408 km
Perigee altitude
496.899 km
Semi-major axis
6,878.791 km
Eccentricity
0.00055
Inclination
34.9956°
RAAN
246.5175°
Arg. of periapsis
195.3524°
True anomaly
164.71909°
Mean anomaly
164.7026°
Eccentric anomaly
164.71085°
Mean motion
3.8043 °/min
Orbital period
94.63 mins
BSTAR
-0.0000040798
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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 | 2025-12-23 18:44:51.638Z | 190.184° SSW | 2025-12-23 18:46:51.638Z | 158.575° S | 14.36° | 2025-12-23 18:48:51.638Z | 125.33° SE |
| 5 mins | 2025-12-23 20:23:51.638Z | 226.028° WSW | 2025-12-23 20:25:51.638Z | 185.198° SSW | 27.859° | 2025-12-23 20:28:51.638Z | 112.71° SE |
| 5 mins | 2025-12-23 22:03:51.638Z | 239.013° WSW | 2025-12-23 22:05:51.638Z | 183.101° SSW | 31.238° | 2025-12-23 22:08:51.638Z | 120.278° SE |
| 4 mins | 2025-12-23 23:43:51.638Z | 227.684° WSW | 2025-12-23 23:44:51.638Z | 207.413° SW | 19.041° | 2025-12-23 23:47:51.638Z | 153.385° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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