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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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: 15 hours ago
TLE from 15 hours ago
0 YAOGAN-30 E
1 43029U 17075B 26098.10278005 .00002881 00000-0 21564-3 0 9996
2 43029 34.9955 337.2860 0003856 328.2349 31.8126 15.02337248456817Epoch: 2026-04-08T02:28Z
TLE epoch observation values (Epoch: 2026-04-08T02:28:00.196Z)
Latitude
-0.00002°
Longitude
103.9152°
Altitude
556.335 km
Speed
7.587 km/s
True Right ascension
22h 29m 08s
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
23:44:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
565.589 km
Perigee altitude
560.236 km
Semi-major axis
6,941.05 km
Eccentricity
0.00039
Inclination
34.9955°
RAAN
337.286°
Arg. of periapsis
328.2349°
True anomaly
31.8359°
Mean anomaly
31.8126°
Eccentric anomaly
31.82425°
Mean motion
3.75323 °/min
Orbital period
95.92 mins
BSTAR
0.00021564
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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 | 2026-04-08 20:17:39.886Z | 203.21° SW | 2026-04-08 20:19:39.886Z | 155.265° SSE | 25.717° | 2026-04-08 20:22:39.886Z | 106.401° ESE |
| 6 mins | 2026-04-08 21:57:39.886Z | 241.574° WSW | 2026-04-08 22:00:39.886Z | 161.266° S | 33.056° | 2026-04-08 22:03:39.886Z | 111.512° ESE |
| 6 mins | 2026-04-08 23:38:39.886Z | 244.965° WSW | 2026-04-08 23:40:39.886Z | 206.928° SW | 25.841° | 2026-04-08 23:44:39.886Z | 135.037° SSE |
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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