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: 13 hours ago
TLE from 13 hours ago
0 YAOGAN-30 E
1 43029U 17075B 26008.10346221 .00003295 00000-0 25053-3 0 9990
2 43029 34.9926 165.2685 0003859 276.1504 83.8764 15.01688562443274Epoch: 2026-01-08T02:28Z
TLE epoch observation values (Epoch: 2026-01-08T02:28:59.134Z)
Latitude
-0.00004°
Longitude
20.35968°
Altitude
560.321 km
Speed
7.584 km/s
True Right ascension
11h 01m 04s
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
15:21:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
567.589 km
Perigee altitude
562.231 km
Semi-major axis
6,943.047 km
Eccentricity
0.00039
Inclination
34.9926°
RAAN
165.2685°
Arg. of periapsis
276.1504°
True anomaly
83.92037°
Mean anomaly
83.8764°
Eccentric anomaly
83.89839°
Mean motion
3.75161 °/min
Orbital period
95.96 mins
BSTAR
0.00025053
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-01-08 15:32:24.535Z | 235.449° WSW | 2026-01-08 15:35:24.535Z | 183.797° SSW | 30.794° | 2026-01-08 15:39:24.535Z | 104.895° ESE |
| 6 mins | 2026-01-08 17:14:24.535Z | 243.981° WSW | 2026-01-08 17:16:24.535Z | 199.393° SSW | 32.111° | 2026-01-08 17:20:24.535Z | 118.819° SE |
| 5 mins | 2026-01-08 18:55:24.535Z | 239.598° WSW | 2026-01-08 18:57:24.535Z | 204.874° SW | 19.791° | 2026-01-08 19:00:24.535Z | 155.514° SSE |
| 5 mins | 2026-01-09 13:50:24.535Z | 195.511° SSW | 2026-01-09 13:52:24.535Z | 156.706° SSE | 21.186° | 2026-01-09 13:55:24.535Z | 109.31° ESE |
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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