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: 5 hours ago
TLE from 5 hours ago
0 YAOGAN-43 02E
1 60949U 24156E 25324.33887220 .00019088 00000-0 78698-3 0 9992
2 60949 34.9967 71.6082 0005900 331.2042 28.8347 15.23194163 67584Epoch: 2025-11-20T08:07Z
TLE epoch observation values (Epoch: 2025-11-20T08:07:58.558Z)
Latitude
0.00003°
Longitude
-109.98343°
Altitude
491.568 km
Speed
7.623 km/s
True Right ascension
04h 46m 25s
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
10:33:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.522 km
Perigee altitude
495.407 km
Semi-major axis
6,877.601 km
Eccentricity
0.00059
Inclination
34.9967°
RAAN
71.6082°
Arg. of periapsis
331.2042°
True anomaly
28.86733°
Mean anomaly
28.8347°
Eccentric anomaly
28.85101°
Mean motion
3.80529 °/min
Orbital period
94.61 mins
BSTAR
0.00078698
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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 | 2025-11-20 14:49:39.290Z | 251.783° W | 2025-11-20 14:52:39.290Z | 192.234° SSW | 27.932° | 2025-11-20 14:55:39.290Z | 130.608° SE |
| 4 mins | 2025-11-21 11:08:39.290Z | 187.128° SSW | 2025-11-21 11:09:39.290Z | 164.813° S | 20.543° | 2025-11-21 11:12:39.290Z | 111.013° ESE |
| 6 mins | 2025-11-21 12:46:39.290Z | 237.422° WSW | 2025-11-21 12:49:39.290Z | 157.004° SSE | 30.609° | 2025-11-21 12:52:39.290Z | 108.057° 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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