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: 6 days ago
TLE from 6 days ago
0 YAOGAN-43 02E
1 60949U 24156E 25252.16864552 .00016232 00000-0 67100-3 0 9990
2 60949 34.9967 165.5264 0001979 272.1066 87.9422 15.23141737 56576Epoch: 2025-09-09T04:02Z
TLE epoch observation values (Epoch: 2025-09-09T04:02:50.972Z)
Latitude
-0.00004°
Longitude
116.35068°
Altitude
495.229 km
Speed
7.619 km/s
True Right ascension
11h 02m 06s
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
05:46:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.983 km
Perigee altitude
498.261 km
Semi-major axis
6,877.759 km
Eccentricity
0.0002
Inclination
34.9967°
RAAN
165.5264°
Arg. of periapsis
272.1066°
True anomaly
87.96486°
Mean anomaly
87.9422°
Eccentric anomaly
87.95353°
Mean motion
3.80516 °/min
Orbital period
94.61 mins
BSTAR
0.000671
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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 | 2025-09-15 19:09:18.723Z | 199.847° SSW | 2025-09-15 19:11:18.723Z | 165.636° S | 17.697° | 2025-09-15 19:14:18.723Z | 113.757° SE |
| 5 mins | 2025-09-15 20:49:18.723Z | 221.695° SW | 2025-09-15 20:51:18.723Z | 159.562° S | 30.031° | 2025-09-15 20:54:18.723Z | 107.148° ESE |
| 5 mins | 2025-09-15 22:28:18.723Z | 241.968° WSW | 2025-09-15 22:30:18.723Z | 192.331° SSW | 29.237° | 2025-09-15 22:33:18.723Z | 127.299° 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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