YAOGAN-30 F, 43030
Orbit data source: Space-Track
YAOGAN-30 F, 43030 is a payload satellite owned by PLA SSF (CN) in LEO that was launched on Fri, 24 Nov 2017 UTC via a CHANG ZHENG 2C 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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43030 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
Mission
Operational Defense Sigint
Bus & Motor
Unknown
Mass
~500 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.446 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 YAOGAN-30 F
1 43030U 17075C 26172.50243912 .00001695 00000-0 12665-3 0 9998
2 43030 34.9944 243.9033 0001615 89.0040 271.0853 15.02677714468074Epoch: 2026-06-21T12:03Z
TLE epoch observation values (Epoch: 2026-06-21T12:03:30.739Z)
Latitude
-0.00005°
Longitude
153.32337°
Altitude
557.539 km
Speed
7.585 km/s
True Right ascension
16h 15m 36s
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
21:40:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.986 km
Perigee altitude
560.745 km
Semi-major axis
6,940.002 km
Eccentricity
0.00016
Inclination
34.9944°
RAAN
243.9033°
Arg. of periapsis
89.004°
True anomaly
271.0668°
Mean anomaly
271.0853°
Eccentric anomaly
271.07605°
Mean motion
3.75408 °/min
Orbital period
95.9 mins
BSTAR
0.00012665
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Other satellites on launch #75 in the year 2017 (2017-11-24 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-30 F 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-22 10:42:48.153Z | 249.75° W | 2026-06-22 10:46:48.153Z | 172.955° S | 33.729° | 2026-06-22 10:49:48.153Z | 112.909° SE |
| 5 mins | 2026-06-22 12:25:48.153Z | 235.084° WSW | 2026-06-22 12:27:48.153Z | 186.507° SSW | 26.342° | 2026-06-22 12:30:48.153Z | 136.178° SSE |
| 6 mins | 2026-06-23 08:59:48.153Z | 219.713° SW | 2026-06-23 09:01:48.153Z | 177.737° S | 28.411° | 2026-06-23 09:05:48.153Z | 103.938° ESE |
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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