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 | 14 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 14 hours ago
0 YAOGAN-39 04C
1 58145U 23163E 24348.07656708 .00017427 00000-0 72088-3 0 9997
2 58145 34.9929 210.5375 0003149 349.8502 10.2149 15.23106677 63501
Epoch: 2024-12-13T01:50Z
Definitive object data (Epoch: 2024-12-13T01:50:15.395Z)
Latitude | -0° |
Longitude | 100.72562° |
Altitude | 493.253 km |
Speed | 7.622 km/s |
True Right ascension | 14h 02m 08s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -7.96719° |
Longitude | 85.5623° |
Altitude | 494.563 km |
Speed | 7.62 km/s |
Apparent Right ascension | 10h 27m 34s |
Apparent Declination | -60° 15' 16" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 14:26:56 |
Azimuth | 207.449° SW |
Elevation | -21.465° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 501.894 km |
Perigee altitude | 497.562 km |
Semi-major axis | 6,877.865 km |
Eccentricity | 0.0003149 |
Inclination | 34.9929° |
RAAN | 210.5375° |
Arg. of periapsis | 349.8502° |
True anomaly | 10.2213° |
Mean anomaly | 10.2149° |
Eccentric anomaly | 10.2181° |
Mean motion | 3.80507 °/min |
BSTAR | 0.00072088 |
Orbital period | 94.61 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. |
---|---|---|---|---|---|---|---|
5 mins | 2024-12-13 19:24:05.986Z | 217.374° SW | 2024-12-13 19:27:05.986Z | 157.343° SSE | 23.413° | 2024-12-13 19:29:05.986Z | 116.865° SE |
5 mins | 2024-12-13 21:04:05.986Z | 237.571° WSW | 2024-12-13 21:06:05.986Z | 186.68° SSW | 31.972° | 2024-12-13 21:09:05.986Z | 114.922° SE |
4 mins | 2024-12-13 22:44:05.986Z | 233.876° WSW | 2024-12-13 22:46:05.986Z | 183.345° SSW | 24.323° | 2024-12-13 22:48:05.986Z | 143.966° SSE |
Authenticating...
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