YAOGAN-43 03A, 61617
Orbit data source: Space-Track
YAOGAN-43 03A, 61617 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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61617 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: 9 hours ago
TLE from 9 hours ago
0 YAOGAN-43 03A
1 61617U 24190A 26098.89239166 .00006140 00000-0 25427-3 0 9990
2 61617 34.9905 273.5631 0004676 55.5265 304.5891 15.23245371 81294Epoch: 2026-04-08T21:25Z
TLE epoch observation values (Epoch: 2026-04-08T21:25:02.639Z)
Latitude
-0.00001°
Longitude
115.15386°
Altitude
493.142 km
Speed
7.622 km/s
True Right ascension
18h 14m 15s
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
12:53:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.527 km
Perigee altitude
496.095 km
Semi-major axis
6,877.448 km
Eccentricity
0.00047
Inclination
34.9905°
RAAN
273.5631°
Arg. of periapsis
55.5265°
True anomaly
304.54497°
Mean anomaly
304.5891°
Eccentric anomaly
304.56704°
Mean motion
3.80542 °/min
Orbital period
94.6 mins
BSTAR
0.00025427
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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 03A 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 | 2026-04-09 14:56:46.292Z | 187.233° SSW | 2026-04-09 14:58:46.292Z | 153.693° SSE | 14.419° | 2026-04-09 15:00:46.292Z | 121.476° SE |
| 5 mins | 2026-04-09 16:35:46.292Z | 222.974° SW | 2026-04-09 16:37:46.292Z | 174.905° S | 28.45° | 2026-04-09 16:40:46.292Z | 109.753° ESE |
| 5 mins | 2026-04-09 18:15:46.292Z | 233.538° WSW | 2026-04-09 18:17:46.292Z | 169.609° S | 30.168° | 2026-04-09 18:20:46.292Z | 118.41° 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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