YAOGAN-30 E, 43029
Orbit data source: Space-Track
YAOGAN-30 E, 43029 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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43029 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: 6 hours ago
TLE from 6 hours ago
0 YAOGAN-30 E
1 43029U 17075B 25347.03982603 .00006003 00000-0 45686-3 0 9991
2 43029 34.9956 323.8564 0002293 24.0673 336.0142 15.01489237439358Epoch: 2025-12-13T00:57Z
TLE epoch observation values (Epoch: 2025-12-13T00:57:20.968Z)
Latitude
-0.00002°
Longitude
-132.45381°
Altitude
559.767 km
Speed
7.585 km/s
True Right ascension
21h 35m 25s
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
05:28:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
567.116 km
Perigee altitude
563.931 km
Semi-major axis
6,943.661 km
Eccentricity
0.00023
Inclination
34.9956°
RAAN
323.8564°
Arg. of periapsis
24.0673°
True anomaly
336.00352°
Mean anomaly
336.0142°
Eccentric anomaly
336.00886°
Mean motion
3.75112 °/min
Orbital period
95.97 mins
BSTAR
0.00045686
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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 E 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 | 2025-12-13 07:50:18.279Z | 242.506° WSW | 2025-12-13 07:53:18.279Z | 196.647° SSW | 15.416° | 2025-12-13 07:55:18.279Z | 167.825° S |
| 6 mins | 2025-12-14 02:45:18.279Z | 211.902° SW | 2025-12-14 02:47:18.279Z | 174.583° S | 24.779° | 2025-12-14 02:51:18.279Z | 104.731° ESE |
| 6 mins | 2025-12-14 04:26:18.279Z | 238.623° WSW | 2025-12-14 04:28:18.279Z | 193.028° SSW | 33.412° | 2025-12-14 04:32:18.279Z | 109.577° ESE |
| 6 mins | 2025-12-14 06:07:18.279Z | 243.591° WSW | 2025-12-14 06:09:18.279Z | 202.783° SW | 26.875° | 2025-12-14 06:13:18.279Z | 132.368° SE |
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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