YAOGAN-43 02F, 60950
Orbit data source: Space-Track
YAOGAN-43 02F, 60950 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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60950 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 YAOGAN-43 02F
1 60950U 24156F 26306.75479426 .00005404 00000-0 22523-3 0 9999
2 60950 34.9941 46.3636 0001491 154.1671 205.9118 15.23069360120587Epoch: 2026-11-02T18:06Z
TLE epoch observation values (Epoch: 2026-11-02T18:06:54.224Z)
Latitude
-0.00001°
Longitude
92.61038°
Altitude
496.417 km
Speed
7.618 km/s
True Right ascension
03h 05m 27s
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
21:43:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.866 km
Perigee altitude
498.815 km
Semi-major axis
6,877.977 km
Eccentricity
0.00015
Inclination
34.9941°
RAAN
46.3636°
Arg. of periapsis
154.1671°
True anomaly
205.90434°
Mean anomaly
205.9118°
Eccentric anomaly
205.90807°
Mean motion
3.80498 °/min
Orbital period
94.61 mins
BSTAR
0.00022523
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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 02F 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 | 2026-11-03 11:43:11.910Z | 219.854° SW | 2026-11-03 11:45:11.910Z | 169.682° S | 32.705° | 2026-11-03 11:48:11.910Z | 108.289° ESE |
| 6 mins | 2026-11-03 13:22:11.910Z | 245.516° WSW | 2026-11-03 13:24:11.910Z | 204.113° SW | 36.436° | 2026-11-03 13:28:11.910Z | 116.145° SE |
| 4 mins | 2026-11-03 15:02:11.910Z | 236.82° WSW | 2026-11-03 15:04:11.910Z | 196.258° SSW | 21.357° | 2026-11-03 15:06:11.910Z | 158.169° 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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