YAOGAN-43 03C, 61619
Orbit data source: Space-Track
YAOGAN-43 03C, 61619 is a payload satellite owned by PLA GAD (CN) in LEO that was launched on Wed, 23 Oct 2024 UTC via a CHANG ZHENG 2C 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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61619 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Operational Defense Communications
Bus & Motor
Unknown
Mass
~300 kg wet, ~300 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.5 m
Radar Cross Section
11.063 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 YAOGAN-43 03C
1 61619U 24190C 25355.86900054 .00002408 00000-0 10164-3 0 9990
2 61619 34.9954 233.2511 0006676 193.6686 166.3848 15.22916471 64778Epoch: 2025-12-21T20:51Z
TLE epoch observation values (Epoch: 2025-12-21T20:51:21.646Z)
Latitude
-0.00005°
Longitude
-170.26443°
Altitude
500.416 km
Speed
7.614 km/s
True Right ascension
15h 33m 00s
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
00:57:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.892 km
Perigee altitude
495.708 km
Semi-major axis
6,878.437 km
Eccentricity
0.00067
Inclination
34.9954°
RAAN
233.2511°
Arg. of periapsis
193.6686°
True anomaly
166.40279°
Mean anomaly
166.3848°
Eccentric anomaly
166.3938°
Mean motion
3.8046 °/min
Orbital period
94.62 mins
BSTAR
0.00010164
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Other satellites on launch #190 in the year 2024 (2024-10-23 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-43 03C 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-22 20:45:17.258Z | 217.455° SW | 2025-12-22 20:47:17.258Z | 166.94° S | 27.711° | 2025-12-22 20:50:17.258Z | 108.078° ESE |
| 5 mins | 2025-12-22 22:24:17.258Z | 244.184° WSW | 2025-12-22 22:26:17.258Z | 201.172° SSW | 30.772° | 2025-12-22 22:29:17.258Z | 122.574° SE |
| 4 mins | 2025-12-23 00:04:17.258Z | 236.003° WSW | 2025-12-23 00:06:17.258Z | 194.654° SSW | 20.2° | 2025-12-23 00:08:17.258Z | 156.738° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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