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: 6 hours ago
TLE from 6 hours ago
0 YAOGAN-43 02C
1 60947U 24156C 26310.62125406 .00006801 00000-0 28317-3 0 9991
2 60947 34.9996 22.3562 0003844 240.6029 119.4303 15.23043753121176Epoch: 2026-11-06T14:54Z
TLE epoch observation values (Epoch: 2026-11-06T14:54:36.350Z)
Latitude
0.00003°
Longitude
112.86655°
Altitude
496.872 km
Speed
7.618 km/s
True Right ascension
01h 29m 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
17:19:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.56 km
Perigee altitude
497.272 km
Semi-major axis
6,878.053 km
Eccentricity
0.00038
Inclination
34.9996°
RAAN
22.3562°
Arg. of periapsis
240.6029°
True anomaly
119.46866°
Mean anomaly
119.4303°
Eccentric anomaly
119.44948°
Mean motion
3.80491 °/min
Orbital period
94.61 mins
BSTAR
0.00028317
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-07 08:26:29.952Z | 196.108° SSW | 2026-11-07 08:28:29.952Z | 163.539° S | 16.953° | 2026-11-07 08:30:29.952Z | 126.988° SE |
| 5 mins | 2026-11-07 10:06:29.952Z | 218.714° SW | 2026-11-07 10:08:29.952Z | 158.084° S | 34.594° | 2026-11-07 10:11:29.952Z | 106.053° ESE |
| 5 mins | 2026-11-07 11:45:29.952Z | 242.426° WSW | 2026-11-07 11:47:29.952Z | 191.82° SSW | 36.55° | 2026-11-07 11:50:29.952Z | 123.999° SE |
| 4 mins | 2026-11-07 13:25:29.952Z | 229.841° WSW | 2026-11-07 13:26:29.952Z | 211.216° SW | 18.236° | 2026-11-07 13:29:29.952Z | 158.49° S |
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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