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: 9 hours ago
TLE from 9 hours ago
0 YAOGAN-30 F
1 43030U 17075C 25261.95036788 .00003003 00000-0 23542-3 0 9997
2 43030 34.9943 121.1239 0002290 231.5190 128.5313 15.00560817426623Epoch: 2025-09-18T22:48Z
TLE epoch observation values (Epoch: 2025-09-18T22:48:31.784Z)
Latitude
0.00001°
Longitude
140.88687°
Altitude
565.074 km
Speed
7.58 km/s
True Right ascension
08h 04m 29s
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
00:35:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
569.976 km
Perigee altitude
566.794 km
Semi-major axis
6,946.522 km
Eccentricity
0.00023
Inclination
34.9943°
RAAN
121.1239°
Arg. of periapsis
231.519°
True anomaly
128.55182°
Mean anomaly
128.5313°
Eccentric anomaly
128.54156°
Mean motion
3.7488 °/min
Orbital period
96.03 mins
BSTAR
0.00023542
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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 | 2025-09-19 18:11:37.854Z | 201.338° SSW | 2025-09-19 18:14:37.854Z | 153.766° SSE | 18.459° | 2025-09-19 18:16:37.854Z | 120.633° SE |
| 6 mins | 2025-09-19 19:52:37.854Z | 232.116° WSW | 2025-09-19 19:55:37.854Z | 160.893° S | 31.608° | 2025-09-19 19:58:37.854Z | 107.287° ESE |
| 6 mins | 2025-09-19 21:33:37.854Z | 248.356° W | 2025-09-19 21:36:37.854Z | 178.352° S | 31.844° | 2025-09-19 21:39:37.854Z | 123.037° SE |
| 4 mins | 2025-09-19 23:15:37.854Z | 231.782° WSW | 2025-09-19 23:17:37.854Z | 195.14° SSW | 18.563° | 2025-09-19 23:19:37.854Z | 163.043° 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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