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: 2 hours ago
TLE from 2 hours ago
0 YAOGAN-43 02E
1 60949U 24156E 26052.55711253 .00013344 00000-0 55456-3 0 9993
2 60949 34.9954 205.4056 0006809 338.0414 22.0008 15.22975068 81806Epoch: 2026-02-21T13:22Z
TLE epoch observation values (Epoch: 2026-02-21T13:22:14.522Z)
Latitude
-0.00003°
Longitude
-146.63294°
Altitude
491.44 km
Speed
7.624 km/s
True Right ascension
13h 41m 37s
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
18:56:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.807 km
Perigee altitude
495.44 km
Semi-major axis
6,878.26 km
Eccentricity
0.00068
Inclination
34.9954°
RAAN
205.4056°
Arg. of periapsis
338.0414°
True anomaly
22.03005°
Mean anomaly
22.0008°
Eccentric anomaly
22.01542°
Mean motion
3.80474 °/min
Orbital period
94.62 mins
BSTAR
0.00055456
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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 | 2026-02-21 16:52:53.669Z | 248.15° W | 2026-02-21 16:55:53.669Z | 179.996° S | 31.687° | 2026-02-21 16:58:53.669Z | 117.84° SE |
| 4 mins | 2026-02-21 18:33:53.669Z | 227.516° WSW | 2026-02-21 18:34:53.669Z | 205.988° SW | 20.634° | 2026-02-21 18:37:53.669Z | 149.746° SSE |
| 5 mins | 2026-02-22 14:50:53.669Z | 212.487° SW | 2026-02-22 14:52:53.669Z | 155.806° SSE | 27.276° | 2026-02-22 14:55:53.669Z | 105.582° ESE |
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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