YAOGAN-39 04C, 58145
Orbit data source: Space-Track
YAOGAN-39 04C, 58145 is a payload satellite owned by PLA GAD (CN) in LEO that was launched on Mon, 23 Oct 2023 UTC via a CHANG ZHENG 2D launch vehicle from the Xichang Space Center, China (XSC). 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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58145 intel report (Beta)
YAOGAN-39 04C details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 6 hours ago |
| Origin | |
| Manufacturer | DFH |
| Mission | Operational Defense Sigint |
| Bus & Motor | Unknown |
| Mass | ~300 kg wet, ~300 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 | 11.063 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 6 hours ago
0 YAOGAN-39 04C
1 58145U 23163E 24356.46777631 .00017595 00000-0 72941-3 0 9992
2 58145 34.9926 157.7683 0002261 24.7727 335.3096 15.23034006 64783Epoch: 2024-12-21T11:13Z
Definitive object data (Epoch: 2024-12-21T11:13:35.873Z)
| Latitude | 0° |
| Longitude | -101.14968° |
| Altitude | 494.19 km |
| Speed | 7.621 km/s |
| True Right ascension | 10h 31m 04s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -15.42437° |
| Longitude | -125.84421° |
| Altitude | 497.927 km |
| Speed | 7.618 km/s |
| Apparent Right ascension | 07h 01m 53s |
| Apparent Declination | -31° 16' 59" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 16:26:34 |
| Azimuth | 273.089° WNW |
| Elevation | -57.546° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 501.502 km |
| Perigee altitude | 498.392 km |
| Semi-major axis | 6,878.084 km |
| Eccentricity | 0.0002261 |
| Inclination | 34.9926° |
| RAAN | 157.7683° |
| Arg. of periapsis | 24.7727° |
| True anomaly | 335.29877° |
| Mean anomaly | 335.3096° |
| Eccentric anomaly | 335.30419° |
| Mean motion | 3.80489 °/min |
| BSTAR | 0.00072941 |
| Orbital period | 94.62 mins |
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Other satellites on launch #163 in the year 2023 (2023-10-23 UTC)
| YAOGAN-39 04A, 58141 |
| CZ-2D R/B, 58142 (Decayed) |
| YAOGAN-39 04B, 58143 |
| CZ-2D DEB, 58144 (Decayed) |
| YAOGAN-39 04C, 58145 |
YAOGAN-39 04C 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2024-12-21 17:52:57.876Z | 253.267° W | 2024-12-21 17:56:57.876Z | 167.39° S | 30.153° | 2024-12-21 17:59:57.876Z | 117.81° SE |
| 5 mins | 2024-12-22 15:50:57.876Z | 224.301° SW | 2024-12-22 15:52:57.876Z | 176.526° S | 28.844° | 2024-12-22 15:55:57.876Z | 110.092° ESE |
Authenticating...
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