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: 16 hours ago
TLE from 16 hours ago
0 YAOGAN-43 02E
1 60949U 24156E 26126.36606984 .00010214 00000-0 42170-3 0 9990
2 60949 34.9952 101.1794 0002856 264.9040 95.1349 15.23256048 93066Epoch: 2026-05-06T08:47Z
TLE epoch observation values (Epoch: 2026-05-06T08:47:08.434Z)
Latitude
0.00001°
Longitude
105.16668°
Altitude
495.11 km
Speed
7.619 km/s
True Right ascension
06h 44m 43s
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
09:10:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.243 km
Perigee altitude
497.314 km
Semi-major axis
6,877.415 km
Eccentricity
0.00029
Inclination
34.9952°
RAAN
101.1794°
Arg. of periapsis
264.904°
True anomaly
95.16749°
Mean anomaly
95.1349°
Eccentric anomaly
95.1512°
Mean motion
3.80544 °/min
Orbital period
94.6 mins
BSTAR
0.0004217
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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 | 2026-05-07 02:19:53.617Z | 212.227° SW | 2026-05-07 02:22:53.617Z | 157.82° S | 20.862° | 2026-05-07 02:24:53.617Z | 119.009° SE |
| 5 mins | 2026-05-07 03:59:53.617Z | 234.682° WSW | 2026-05-07 04:01:53.617Z | 185.719° SSW | 31.509° | 2026-05-07 04:04:53.617Z | 113.023° SE |
| 5 mins | 2026-05-07 05:39:53.617Z | 235.574° WSW | 2026-05-07 05:41:53.617Z | 181.38° SSW | 26.836° | 2026-05-07 05:44:53.617Z | 129.603° 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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