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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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: 5 hours ago
TLE from 5 hours ago
0 YAOGAN 1
1 29092U 06015A 26071.57926060 .00001155 00000-0 13302-3 0 9999
2 29092 97.7553 94.7485 0001495 94.6546 265.4841 14.87592381 75448Epoch: 2026-03-12T13:54Z
TLE epoch observation values (Epoch: 2026-03-12T13:54:08.115Z)
Latitude
-0.00007°
Longitude
75.98758°
Altitude
608.579 km
Speed
7.555 km/s
True Right ascension
06h 18m 59s
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
23:20:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
603.529 km
Perigee altitude
601.441 km
Semi-major axis
6,980.622 km
Eccentricity
0.00015
Inclination
97.7553°
RAAN
94.7485°
Arg. of periapsis
94.6546°
True anomaly
265.46702°
Mean anomaly
265.4841°
Eccentric anomaly
265.47556°
Mean motion
3.72136 °/min
Orbital period
96.74 mins
BSTAR
0.00013302
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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
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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 | 2026-03-13 01:19:18.746Z | 158.049° S | 2026-03-13 01:23:18.746Z | 50.831° ENE | 42.95° | 2026-03-13 01:26:18.746Z | 354.228° N |
| 7 mins | 2026-03-13 14:41:18.746Z | 357.74° N | 2026-03-13 14:44:18.746Z | 286.23° WNW | 38.494° | 2026-03-13 14:48:18.746Z | 210.228° SW |
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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