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: 1 day ago
TLE from 1 day ago
0 YAOGAN-43 03C
1 61619U 24190C 25340.66213148 .00005768 00000-0 23964-3 0 9997
2 61619 34.9971 328.9033 0005294 42.5356 317.5768 15.23150969 62456Epoch: 2025-12-06T15:53Z
TLE epoch observation values (Epoch: 2025-12-06T15:53:28.159Z)
Latitude
-0.00004°
Longitude
14.84926°
Altitude
492.565 km
Speed
7.622 km/s
True Right ascension
21h 55m 36s
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
15:05:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.235 km
Perigee altitude
495.953 km
Semi-major axis
6,877.731 km
Eccentricity
0.00053
Inclination
34.9971°
RAAN
328.9033°
Arg. of periapsis
42.5356°
True anomaly
317.53586°
Mean anomaly
317.5768°
Eccentric anomaly
317.55633°
Mean motion
3.80518 °/min
Orbital period
94.61 mins
BSTAR
0.00023964
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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 | 2025-12-08 02:43:42.053Z | 203.853° SW | 2025-12-08 02:46:42.053Z | 151.969° SSE | 17.498° | 2025-12-08 02:48:42.053Z | 117.905° SE |
| 5 mins | 2025-12-08 04:23:42.053Z | 227.227° WSW | 2025-12-08 04:25:42.053Z | 173.564° S | 30.444° | 2025-12-08 04:28:42.053Z | 109.588° ESE |
| 4 mins | 2025-12-08 06:03:42.053Z | 231.976° WSW | 2025-12-08 06:04:42.053Z | 205.503° SW | 28.388° | 2025-12-08 06:07:42.053Z | 130.545° SE |
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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