YAOGAN-43 02A, 60945
Orbit data source: Space-Track
YAOGAN-43 02A, 60945 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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60945 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: 1 day ago
TLE from 1 day ago
0 YAOGAN-43 02A
1 60945U 24156A 25315.15859728 .00045900 00000-0 14310-2 0 9992
2 60945 34.9961 121.6082 0005150 24.4312 335.6648 15.32187435 66315Epoch: 2025-11-11T03:48Z
TLE epoch observation values (Epoch: 2025-11-11T03:48:22.804Z)
Latitude
-0.00009°
Longitude
13.9639°
Altitude
464.978 km
Speed
7.638 km/s
True Right ascension
08h 06m 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
06:08:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.079 km
Perigee altitude
469.023 km
Semi-major axis
6,850.688 km
Eccentricity
0.00052
Inclination
34.9961°
RAAN
121.6082°
Arg. of periapsis
24.4312°
True anomaly
335.64047°
Mean anomaly
335.6648°
Eccentric anomaly
335.65264°
Mean motion
3.82774 °/min
Orbital period
94.05 mins
BSTAR
0.001431
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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 02A 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 | 2025-11-12 16:04:53.082Z | 227.417° WSW | 2025-11-12 16:06:53.082Z | 179.676° S | 28.552° | 2025-11-12 16:09:53.082Z | 110.561° ESE |
| 5 mins | 2025-11-12 17:43:53.082Z | 241.26° WSW | 2025-11-12 17:45:53.082Z | 189.071° SSW | 29.194° | 2025-11-12 17:48:53.082Z | 123.97° SE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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