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 25261.97224199 .00002936 00000-0 22972-3 0 9992
2 43029 34.9930 121.0544 0003605 6.2624 353.8128 15.00646699426568Epoch: 2025-09-18T23:20Z
TLE epoch observation values (Epoch: 2025-09-18T23:20:01.707Z)
Latitude
-0.00004°
Longitude
132.92106°
Altitude
561.33 km
Speed
7.584 km/s
True Right ascension
08h 04m 13s
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
22:26:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.624 km
Perigee altitude
565.616 km
Semi-major axis
6,946.257 km
Eccentricity
0.00036
Inclination
34.993°
RAAN
121.0544°
Arg. of periapsis
6.2624°
True anomaly
353.80835°
Mean anomaly
353.8128°
Eccentric anomaly
353.81057°
Mean motion
3.74901 °/min
Orbital period
96.03 mins
BSTAR
0.00022972
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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 | 2025-09-19 18:44:04.848Z | 217.452° SW | 2025-09-19 18:47:04.848Z | 171.471° S | 23.194° | 2025-09-19 18:50:04.848Z | 113.868° SE |
| 6 mins | 2025-09-19 20:26:04.848Z | 236.515° WSW | 2025-09-19 20:28:04.848Z | 191.381° SSW | 33.214° | 2025-09-19 20:32:04.848Z | 108.121° ESE |
| 6 mins | 2025-09-19 22:07:04.848Z | 244.927° WSW | 2025-09-19 22:09:04.848Z | 204.295° SW | 28.269° | 2025-09-19 22:13:04.848Z | 129.53° SE |
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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