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: 13 hours ago
TLE from 13 hours ago
0 YAOGAN-30 F
1 43030U 17075C 26278.25732789 .00001757 00000-0 12978-3 0 9998
2 43030 34.9957 319.0834 0002690 290.1157 69.9262 15.03090559483993Epoch: 2026-10-05T06:10Z
TLE epoch observation values (Epoch: 2026-10-05T06:10:33.129Z)
Latitude
-0.00001°
Longitude
-147.49347°
Altitude
555.65 km
Speed
7.586 km/s
True Right ascension
21h 16m 20s
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
13:22:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.462 km
Perigee altitude
558.729 km
Semi-major axis
6,938.733 km
Eccentricity
0.00027
Inclination
34.9957°
RAAN
319.0834°
Arg. of periapsis
290.1157°
True anomaly
69.95516°
Mean anomaly
69.9262°
Eccentric anomaly
69.94068°
Mean motion
3.75511 °/min
Orbital period
95.87 mins
BSTAR
0.00012978
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-06 06:18:29.894Z | 206.225° SW | 2026-10-06 06:21:29.894Z | 160.846° S | 20.339° | 2026-10-06 06:24:29.894Z | 112.486° ESE |
| 6 mins | 2026-10-06 07:59:29.894Z | 235.081° WSW | 2026-10-06 08:02:29.894Z | 167.385° S | 39.341° | 2026-10-06 08:05:29.894Z | 108.255° ESE |
| 6 mins | 2026-10-06 09:40:29.894Z | 248.9° W | 2026-10-06 09:43:29.894Z | 178.778° S | 38.125° | 2026-10-06 09:46:29.894Z | 123.621° SE |
| 4 mins | 2026-10-06 11:22:29.894Z | 229.003° WSW | 2026-10-06 11:23:29.894Z | 211.441° SW | 18.908° | 2026-10-06 11:26:29.894Z | 161.833° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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