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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Edit Public Description
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: 22 hours ago
TLE from 22 hours ago
0 YAOGAN-30 F
1 43030U 17075C 26008.54656938 .00003403 00000-0 25878-3 0 9995
2 43030 34.9935 162.5114 0001592 85.0048 275.0841 15.01673662443406Epoch: 2026-01-08T13:07Z
TLE epoch observation values (Epoch: 2026-01-08T13:07:03.594Z)
Latitude
-0.00005°
Longitude
-142.35276°
Altitude
560.554 km
Speed
7.583 km/s
True Right ascension
10h 50m 02s
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
11:12:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
566.061 km
Perigee altitude
563.851 km
Semi-major axis
6,943.093 km
Eccentricity
0.00016
Inclination
34.9935°
RAAN
162.5114°
Arg. of periapsis
85.0048°
True anomaly
275.06593°
Mean anomaly
275.0841°
Eccentric anomaly
275.07501°
Mean motion
3.75158 °/min
Orbital period
95.96 mins
BSTAR
0.00025878
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-01-09 13:16:23.189Z | 189.263° SSW | 2026-01-09 13:18:23.189Z | 158.485° S | 15.86° | 2026-01-09 13:20:23.189Z | 126.001° SE |
| 5 mins | 2026-01-09 14:57:23.189Z | 218.659° SW | 2026-01-09 14:59:23.189Z | 167.157° S | 30.306° | 2026-01-09 15:02:23.189Z | 108.359° ESE |
| 6 mins | 2026-01-09 16:37:23.189Z | 248.621° W | 2026-01-09 16:40:23.189Z | 180.971° SSW | 32.93° | 2026-01-09 16:43:23.189Z | 120.259° SE |
| 5 mins | 2026-01-09 18:19:23.189Z | 234.014° WSW | 2026-01-09 18:21:23.189Z | 194.496° SSW | 20.937° | 2026-01-09 18:24:23.189Z | 148.642° 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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