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: 14 hours ago
TLE from 14 hours ago
0 YAOGAN-30 E
1 43029U 17075B 25311.72777315 .00005665 00000-0 43538-3 0 9997
2 43029 34.9922 178.6237 0002076 86.8380 273.2565 15.01131320434043Epoch: 2025-11-07T17:27Z
TLE epoch observation values (Epoch: 2025-11-07T17:27:59.600Z)
Latitude
-0.00002°
Longitude
-130.54224°
Altitude
562.242 km
Speed
7.582 km/s
True Right ascension
11h 54m 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
03:48:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
568.068 km
Perigee altitude
565.185 km
Semi-major axis
6,944.764 km
Eccentricity
0.00021
Inclination
34.9922°
RAAN
178.6237°
Arg. of periapsis
86.838°
True anomaly
273.23275°
Mean anomaly
273.2565°
Eccentric anomaly
273.24462°
Mean motion
3.75022 °/min
Orbital period
95.99 mins
BSTAR
0.00043538
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-08 19:15:28.029Z | 214.5° SW | 2025-11-08 19:18:28.029Z | 159.981° S | 24.069° | 2025-11-08 19:21:28.029Z | 108.788° ESE |
| 6 mins | 2025-11-08 20:56:28.029Z | 241.733° WSW | 2025-11-08 20:59:28.029Z | 170.821° S | 33.66° | 2025-11-08 21:02:28.029Z | 111.416° ESE |
| 5 mins | 2025-11-08 22:38:28.029Z | 237.186° WSW | 2025-11-08 22:40:28.029Z | 187.697° SSW | 27.98° | 2025-11-08 22:43:28.029Z | 133.856° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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