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). Payloads include a variety of satellites, spacecraft, and rockets 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)
YAOGAN 29 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 7 hours ago |
| Origin | |
| 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 | Payload Rocket body Debris |
| Shape & HBR | Box + 2 Pan, 5 m |
| Radar Cross Section | 4.795 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 7 hours ago
0 YAOGAN 29
1 41038U 15069A 24361.26768981 .00001292 00000-0 16856-3 0 9993
2 41038 98.0469 16.7882 0001531 26.5987 333.5304 14.82270995490914Epoch: 2024-12-26T06:25Z
Definitive object data (Epoch: 2024-12-26T06:25:28.399Z)
| Latitude | -0.00003° |
| Longitude | -174.82966° |
| Altitude | 624.225 km |
| Speed | 7.547 km/s |
| True Right ascension | 01h 07m 09s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -43.16377° |
| Longitude | -2.09402° |
| Altitude | 639.812 km |
| Speed | 7.536 km/s |
| Apparent Right ascension | 07h 57m 56s |
| Apparent Declination | -84° 24' 39" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 13:16:21 |
| Azimuth | 187.05° SSW |
| Elevation | -38.692° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 620.281 km |
| Perigee altitude | 618.138 km |
| Semi-major axis | 6,997.346 km |
| Eccentricity | 0.0001531 |
| Inclination | 98.0469° |
| RAAN | 16.7882° |
| Arg. of periapsis | 26.5987° |
| True anomaly | 333.52258° |
| Mean anomaly | 333.5304° |
| Eccentric anomaly | 333.52649° |
| Mean motion | 3.70803 °/min |
| BSTAR | 0.00016856 |
| Orbital period | 97.09 mins |
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Other satellites on launch #69 in the year 2015 (2015-11-26 UTC)
| YAOGAN 29, 41038 |
| CZ-4C R/B, 41039 |
| CZ-4C DEB, 42670 |
| CZ-4C DEB, 42671 |
| CZ-4C DEB, 42672 |
| YAOGAN 29 DEB, 42673 |
YAOGAN 29 Visibility forecast
Observer location: undefined°, undefined
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 | 2024-12-26 15:05:35.968Z | 337.541° N | 2024-12-26 15:08:35.968Z | 285.996° WNW | 20.996° | 2024-12-26 15:11:35.968Z | 241.343° WSW |
| 5 mins | 2024-12-27 00:24:35.968Z | 103.384° ESE | 2024-12-27 00:26:35.968Z | 64.889° ENE | 21.658° | 2024-12-27 00:29:35.968Z | 17.695° NNE |
| 5 mins | 2024-12-27 02:00:35.968Z | 222.752° SW | 2024-12-27 02:02:35.968Z | 267.46° W | 25.82° | 2024-12-27 02:05:35.968Z | 319.538° NNW |
| 6 mins | 2024-12-27 13:47:35.968Z | 32.807° NE | 2024-12-27 13:50:35.968Z | 113.258° SE | 36.181° | 2024-12-27 13:53:35.968Z | 170.477° S |
Authenticating...
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