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: 5 hours ago
TLE from 5 hours ago
0 YAOGAN 29
1 41038U 15069A 26034.51815957 .00001040 00000-0 13476-3 0 9992
2 41038 98.0175 62.8510 0002927 92.9029 267.2519 14.82957518550812Epoch: 2026-02-03T12:26Z
TLE epoch observation values (Epoch: 2026-02-03T12:26:08.986Z)
Latitude
-0.00007°
Longitude
102.61562°
Altitude
623.125 km
Speed
7.547 km/s
True Right ascension
04h 11m 24s
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
18:58:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
619.094 km
Perigee altitude
614.999 km
Semi-major axis
6,995.183 km
Eccentricity
0.00029
Inclination
98.0175°
RAAN
62.851°
Arg. of periapsis
92.9029°
True anomaly
267.2184°
Mean anomaly
267.2519°
Eccentric anomaly
267.23515°
Mean motion
3.70975 °/min
Orbital period
97.04 mins
BSTAR
0.00013476
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-02-04 01:30:23.225Z | 153.11° SSE | 2026-02-04 01:34:23.225Z | 83.684° E | 40.677° | 2026-02-04 01:38:23.225Z | 356.012° N |
| 7 mins | 2026-02-04 14:55:23.225Z | 1.217° NNE | 2026-02-04 14:58:23.225Z | 270.463° WNW | 41.277° | 2026-02-04 15:02:23.225Z | 205.485° 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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