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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). 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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Identifier
58145, 2023-163E
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)
2023-10-23 (2 years ago)
Launch vehicle
CHANG ZHENG 2D
Launch site
Xichang Space Center, China (XSC)
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   25129.07746933  .00008047  00000-0  40922-3 0  9995
2 58145  34.9940   7.4583 0003119 120.7366 239.3654 15.16137645 85914
Epoch: 2025-05-09T01:51Z
Definitive object data (Epoch: 2025-05-09T01:51:33.35Z)
Latitude
0.00001°
Longitude
112.43056°
Altitude
517.533 km
Speed
7.606 km/s
True Right ascension
00h 29m 49s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at TLE epoch
Visualization TLE readout
Latitude
-13.27089°
Longitude
91.24218°
Altitude
520.874 km
Speed
7.603 km/s
Apparent Right ascension
01h 10m 57s
Apparent Declination
-31° 40' 27"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
16:13:46
Azimuth
92.007° ESE
Elevation
-52.448°
Doppler factor
1
Orbital elements
Apogee altitude
522.92 km
Perigee altitude
518.617 km
Semi-major axis
6,898.905 km
Eccentricity
0.0003119
Inclination
34.994°
RAAN
7.4583°
Arg. of periapsis
120.7366°
True anomaly
239.33465°
Mean anomaly
239.3654°
Eccentric anomaly
239.35003°
Mean motion
3.78768 °/min
BSTAR
0.00040922
Orbital period
95.05 mins
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Other satellites on launch #163 in the year 2023 (2023-10-23 UTC)

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 mins2025-05-09 19:28:39.793Z196.926° SSW2025-05-09 19:30:39.793Z163.005° S17.647°2025-05-09 19:33:39.793Z113.364° SE
5 mins2025-05-09 21:08:39.793Z226.338° WSW2025-05-09 21:10:39.793Z174.168° S30.828°2025-05-09 21:13:39.793Z109.717° ESE
5 mins2025-05-09 22:48:39.793Z240.36° WSW2025-05-09 22:50:39.793Z187.87° SSW30.305°2025-05-09 22:53:39.793Z125.389° SE
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