YAOGAN-43 02C, 60947
Orbit data source: Space-Track
YAOGAN-43 02C, 60947 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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60947 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 YAOGAN-43 02C
1 60947U 24156C 26126.35675284 .00006850 00000-0 28481-3 0 9996
2 60947 34.9970 101.2047 0004414 337.0036 23.0480 15.23087206 93069Epoch: 2026-05-06T08:33Z
TLE epoch observation values (Epoch: 2026-05-06T08:33:43.445Z)
Latitude
-0.00005°
Longitude
108.5552°
Altitude
492.651 km
Speed
7.622 km/s
True Right ascension
06h 44m 49s
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
09:09:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.822 km
Perigee altitude
496.75 km
Semi-major axis
6,877.923 km
Eccentricity
0.00044
Inclination
34.997°
RAAN
101.2047°
Arg. of periapsis
337.0036°
True anomaly
23.06781°
Mean anomaly
23.048°
Eccentric anomaly
23.05791°
Mean motion
3.80502 °/min
Orbital period
94.61 mins
BSTAR
0.00028481
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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 02C 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 02:06:21.195Z | 202.719° SW | 2026-05-07 02:08:21.195Z | 168.471° S | 18.464° | 2026-05-07 02:11:21.195Z | 114.342° SE |
| 5 mins | 2026-05-07 03:46:21.195Z | 225.074° WSW | 2026-05-07 03:48:21.195Z | 164.553° S | 30.73° | 2026-05-07 03:51:21.195Z | 108.314° ESE |
| 5 mins | 2026-05-07 05:25:21.195Z | 243.686° WSW | 2026-05-07 05:27:21.195Z | 197.704° SSW | 28.559° | 2026-05-07 05:30:21.195Z | 130.009° 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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