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: 8 hours ago
TLE from 8 hours ago
0 YAOGAN-43 03C
1 61619U 24190C 26261.66241924 .00001807 00000-0 76450-4 0 9992
2 61619 34.9971 330.1854 0005486 110.0032 250.1274 15.23031474106088Epoch: 2026-09-18T15:53Z
TLE epoch observation values (Epoch: 2026-09-18T15:53:53.022Z)
Latitude
0.00001°
Longitude
94.1324°
Altitude
496.893 km
Speed
7.618 km/s
True Right ascension
22h 00m 44s
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
16:19:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.727 km
Perigee altitude
496.18 km
Semi-major axis
6,878.091 km
Eccentricity
0.00055
Inclination
34.9971°
RAAN
330.1854°
Arg. of periapsis
110.0032°
True anomaly
250.06829°
Mean anomaly
250.1274°
Eccentric anomaly
250.09784°
Mean motion
3.80488 °/min
Orbital period
94.62 mins
BSTAR
0.00007645
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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 | 2026-09-19 09:29:36.468Z | 221.501° SW | 2026-09-19 09:31:36.468Z | 177.862° S | 31.053° | 2026-09-19 09:34:36.468Z | 110.654° ESE |
| 5 mins | 2026-09-19 11:09:36.468Z | 235.973° WSW | 2026-09-19 11:11:36.468Z | 173.511° S | 38.156° | 2026-09-19 11:14:36.468Z | 116.4° SE |
| 4 mins | 2026-09-19 12:49:36.468Z | 224.73° SW | 2026-09-19 12:50:36.468Z | 202.175° SSW | 22.413° | 2026-09-19 12:53:36.468Z | 147.722° 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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