YAOGAN 1, 29092
Orbit data source: Space-Track
YAOGAN 1, 29092 is a payload satellite owned by PLA GAD (CN) in SSO that was launched on Wed, 26 Apr 2006 UTC via a CHANG ZHENG 4C launch vehicle from the Taiyaun Space Center, China (TSC). 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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29092 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Civil Radar Imaging
Bus & Motor
JB-5, Unknown motor
Mass
2,700 kg wet, ~2,700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 4.0 m
Radar Cross Section
9.231 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 YAOGAN 1
1 29092U 06015A 25334.59835371 .00001005 00000-0 11728-3 0 9990
2 29092 97.7622 355.0557 0001539 92.2333 267.9059 14.87337239 60288Epoch: 2025-11-30T14:21Z
TLE epoch observation values (Epoch: 2025-11-30T14:21:37.760Z)
Latitude
-0.00009°
Longitude
69.93847°
Altitude
609.334 km
Speed
7.555 km/s
True Right ascension
23h 40m 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
20:34:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
604.359 km
Perigee altitude
602.21 km
Semi-major axis
6,981.421 km
Eccentricity
0.00015
Inclination
97.7622°
RAAN
355.0557°
Arg. of periapsis
92.2333°
True anomaly
267.88828°
Mean anomaly
267.9059°
Eccentric anomaly
267.89709°
Mean motion
3.72072 °/min
Orbital period
96.76 mins
BSTAR
0.00011728
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Other satellites on launch #15 in the year 2006 (2006-04-26 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 1 Visibility forecast
Loading observer location...
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 | 2025-12-01 01:48:11.767Z | 187.221° SSW | 2025-12-01 01:50:11.767Z | 241.258° WSW | 40.625° | 2025-12-01 01:54:11.767Z | 338.965° N |
| 4 mins | 2025-12-01 13:34:11.767Z | 62.352° ENE | 2025-12-01 13:36:11.767Z | 102.09° ESE | 20.837° | 2025-12-01 13:38:11.767Z | 136.783° SSE |
| 6 mins | 2025-12-01 15:09:11.767Z | 339.011° N | 2025-12-01 15:11:11.767Z | 302.615° NW | 24.936° | 2025-12-01 15:15:11.767Z | 231.604° WSW |
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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