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: 19 hours ago
TLE from 19 hours ago
0 YAOGAN-43 03C
1 61619U 24190C 25260.03423955 .00004654 00000-0 19411-3 0 9993
2 61619 34.9954 115.9905 0005889 24.0987 336.0003 15.23072723 50157Epoch: 2025-09-17T00:49Z
TLE epoch observation values (Epoch: 2025-09-17T00:49:18.297Z)
Latitude
0.00003°
Longitude
107.44832°
Altitude
491.788 km
Speed
7.623 km/s
True Right ascension
07h 43m 57s
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
12:29:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.88 km
Perigee altitude
495.779 km
Semi-major axis
6,877.967 km
Eccentricity
0.00059
Inclination
34.9954°
RAAN
115.9905°
Arg. of periapsis
24.0987°
True anomaly
335.97283°
Mean anomaly
336.0003°
Eccentric anomaly
335.98657°
Mean motion
3.80499 °/min
Orbital period
94.61 mins
BSTAR
0.00019411
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-17 20:00:43.809Z | 241.137° WSW | 2025-09-17 20:03:43.809Z | 182.685° SSW | 31.013° | 2025-09-17 20:06:43.809Z | 111.84° ESE |
| 5 mins | 2025-09-17 21:41:43.809Z | 235.395° WSW | 2025-09-17 21:43:43.809Z | 178.746° S | 27.752° | 2025-09-17 21:46:43.809Z | 126.822° SE |
| 4 mins | 2025-09-18 17:58:43.809Z | 199.077° SSW | 2025-09-18 18:00:43.809Z | 158.434° S | 19.997° | 2025-09-18 18:02:43.809Z | 119.871° SE |
| 4 mins | 2025-09-18 19:37:43.809Z | 234.186° WSW | 2025-09-18 19:39:43.809Z | 186.613° SSW | 31.075° | 2025-09-18 19:41:43.809Z | 124.607° 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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