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: 11 hours ago
TLE from 11 hours ago
0 YAOGAN-30 F
1 43030U 17075C 25312.10500697 .00004628 00000-0 35551-3 0 9993
2 43030 34.9930 176.2716 0002957 277.9842 82.0530 15.01199218434165Epoch: 2025-11-08T02:31Z
TLE epoch observation values (Epoch: 2025-11-08T02:31:12.602Z)
Latitude
-0.00001°
Longitude
90.92967°
Altitude
561.831 km
Speed
7.583 km/s
True Right ascension
11h 45m 05s
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
10:06:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
568.471 km
Perigee altitude
564.364 km
Semi-major axis
6,944.554 km
Eccentricity
0.0003
Inclination
34.993°
RAAN
176.2716°
Arg. of periapsis
277.9842°
True anomaly
82.08656°
Mean anomaly
82.053°
Eccentric anomaly
82.06978°
Mean motion
3.75039 °/min
Orbital period
95.99 mins
BSTAR
0.00035551
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-08 18:42:57.218Z | 197.401° SSW | 2025-11-08 18:44:57.218Z | 164.713° S | 18.934° | 2025-11-08 18:47:57.218Z | 114.824° SE |
| 6 mins | 2025-11-08 20:23:57.218Z | 227.827° WSW | 2025-11-08 20:25:57.218Z | 179.637° S | 32.098° | 2025-11-08 20:29:57.218Z | 104.572° ESE |
| 6 mins | 2025-11-08 22:04:57.218Z | 242.704° WSW | 2025-11-08 22:06:57.218Z | 195.361° SSW | 31.569° | 2025-11-08 22:10:57.218Z | 120.746° SE |
| 4 mins | 2025-11-08 23:46:57.218Z | 221.864° SW | 2025-11-08 23:47:57.218Z | 203.344° SW | 18.083° | 2025-11-08 23:50:57.218Z | 157.784° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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