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 25309.30146872 .00000524 00000-0 71430-4 0 9997
2 41038 98.0261 332.3456 0002530 60.9510 299.1956 14.82817494537443Epoch: 2025-11-05T07:14Z
TLE epoch observation values (Epoch: 2025-11-05T07:14:06.897Z)
Latitude
-0.00005°
Longitude
179.04077°
Altitude
622.603 km
Speed
7.548 km/s
True Right ascension
22h 09m 22s
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
11:32:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
619.257 km
Perigee altitude
615.718 km
Semi-major axis
6,995.625 km
Eccentricity
0.00025
Inclination
98.0261°
RAAN
332.3456°
Arg. of periapsis
60.951°
True anomaly
299.17029°
Mean anomaly
299.1956°
Eccentric anomaly
299.18294°
Mean motion
3.7094 °/min
Orbital period
97.05 mins
BSTAR
0.00007143
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-06 01:11:57.173Z | 129.556° SE | 2025-11-06 01:13:57.173Z | 84.453° E | 32.921° | 2025-11-06 01:17:57.173Z | 3.905° NNE |
| 4 mins | 2025-11-06 02:48:57.173Z | 241.716° WSW | 2025-11-06 02:50:57.173Z | 273.989° WNW | 15.376° | 2025-11-06 02:52:57.173Z | 302.959° NW |
| 7 mins | 2025-11-06 14:34:57.173Z | 12.741° NNE | 2025-11-06 14:37:57.173Z | 6.641° NNE | 44.976° | 2025-11-06 14:41:57.173Z | 194.049° SSW |
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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