YAOGAN 29, 41038
Orbit data source: Space-Track
YAOGAN 29, 41038 is a payload satellite owned by PLA GAD (CN) in SSO that was launched on Thu, 26 Nov 2015 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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41038 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Operational Defense Radar Imaging
Bus & Motor
JB-9, Unknown motor
Mass
1,040 kg wet, 1,040 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.5 m
Radar Cross Section
4.795 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 YAOGAN 29
1 41038U 15069A 26034.31573775 .00001155 00000-0 14897-3 0 9994
2 41038 98.0176 62.6481 0002922 93.8228 266.3320 14.82957376550782Epoch: 2026-02-03T07:34Z
TLE epoch observation values (Epoch: 2026-02-03T07:34:39.741Z)
Latitude
0.00004°
Longitude
175.48408°
Altitude
623.158 km
Speed
7.547 km/s
True Right ascension
04h 10m 35s
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
17:27:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
619.091 km
Perigee altitude
615.003 km
Semi-major axis
6,995.184 km
Eccentricity
0.00029
Inclination
98.0176°
RAAN
62.6481°
Arg. of periapsis
93.8228°
True anomaly
266.29859°
Mean anomaly
266.332°
Eccentric anomaly
266.31529°
Mean motion
3.70975 °/min
Orbital period
97.04 mins
BSTAR
0.00014897
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Other satellites on launch #69 in the year 2015 (2015-11-26 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 29 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 | 2026-02-04 01:30:52.857Z | 151.728° SSE | 2026-02-04 01:34:52.857Z | 49.27° ENE | 39.996° | 2026-02-04 01:37:52.857Z | 357.609° N |
| 7 mins | 2026-02-04 14:54:52.857Z | 3.228° NNE | 2026-02-04 14:57:52.857Z | 309.698° NW | 40.886° | 2026-02-04 15:01:52.857Z | 206.724° SW |
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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