YAOGAN-43 02B, 60946
Orbit data source: Space-Track
YAOGAN-43 02B, 60946 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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60946 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: 7 hours ago
TLE from 7 hours ago
0 YAOGAN-43 02B
1 60946U 24156B 26008.50024628 .00014526 00000-0 59945-3 0 9999
2 60946 34.9952 122.3489 0005594 92.2539 267.8816 15.23205227 75088Epoch: 2026-01-08T12:00Z
TLE epoch observation values (Epoch: 2026-01-08T12:00:21.278Z)
Latitude
-0.00003°
Longitude
-165.79326°
Altitude
495.231 km
Speed
7.619 km/s
True Right ascension
08h 09m 23s
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
19:11:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.279 km
Perigee altitude
495.584 km
Semi-major axis
6,877.568 km
Eccentricity
0.00056
Inclination
34.9952°
RAAN
122.3489°
Arg. of periapsis
92.2539°
True anomaly
267.81754°
Mean anomaly
267.8816°
Eccentric anomaly
267.84957°
Mean motion
3.80532 °/min
Orbital period
94.6 mins
BSTAR
0.00059945
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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 02B 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 | 2026-01-09 11:53:03.540Z | 210.948° SW | 2026-01-09 11:55:03.540Z | 163.362° S | 25.061° | 2026-01-09 11:58:03.540Z | 107.82° ESE |
| 5 mins | 2026-01-09 13:32:03.540Z | 241.246° WSW | 2026-01-09 13:34:03.540Z | 195.5° SSW | 31.399° | 2026-01-09 13:37:03.540Z | 118.119° SE |
| 4 mins | 2026-01-09 15:12:03.540Z | 235.782° WSW | 2026-01-09 15:14:03.540Z | 189.459° SSW | 22.766° | 2026-01-09 15:16:03.540Z | 149.435° SSE |
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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