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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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: 12 hours ago
TLE from 12 hours ago
0 YAOGAN-43 03C
1 61619U 24190C 26311.28466500 .00002915 00000-0 12233-3 0 9994
2 61619 34.9969 18.0964 0006331 204.3940 155.6475 15.23026356113650Epoch: 2026-11-07T06:49Z
TLE epoch observation values (Epoch: 2026-11-07T06:49:55.055Z)
Latitude
-0.00003°
Longitude
-130.87517°
Altitude
499.59 km
Speed
7.615 km/s
True Right ascension
01h 12m 23s
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
15:22:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.324 km
Perigee altitude
495.614 km
Semi-major axis
6,878.106 km
Eccentricity
0.00063
Inclination
34.9969°
RAAN
18.0964°
Arg. of periapsis
204.394°
True anomaly
155.67739°
Mean anomaly
155.6475°
Eccentric anomaly
155.66245°
Mean motion
3.80487 °/min
Orbital period
94.62 mins
BSTAR
0.00012233
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-08 08:14:59.631Z | 196.684° SSW | 2026-11-08 08:16:59.631Z | 158.248° S | 20.226° | 2026-11-08 08:18:59.631Z | 120.831° SE |
| 5 mins | 2026-11-08 09:53:59.631Z | 232.73° WSW | 2026-11-08 09:55:59.631Z | 186.53° SSW | 37.013° | 2026-11-08 09:58:59.631Z | 112.063° ESE |
| 5 mins | 2026-11-08 11:33:59.631Z | 238.099° WSW | 2026-11-08 11:35:59.631Z | 182.282° SSW | 33.809° | 2026-11-08 11:38:59.631Z | 126.006° 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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