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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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: 7 hours ago
TLE from 7 hours ago
0 YAOGAN-43 03A
1 61617U 24190A 25312.53466145 .00010564 00000-0 43952-3 0 9996
2 61617 34.9890 145.5473 0004282 127.2331 232.8774 15.22985824 58204Epoch: 2025-11-08T12:49Z
TLE epoch observation values (Epoch: 2025-11-08T12:49:54.749Z)
Latitude
-0.00004°
Longitude
-94.89377°
Altitude
497.523 km
Speed
7.617 km/s
True Right ascension
09h 42m 11s
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
16:00:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.037 km
Perigee altitude
497.147 km
Semi-major axis
6,878.229 km
Eccentricity
0.00043
Inclination
34.989°
RAAN
145.5473°
Arg. of periapsis
127.2331°
True anomaly
232.83829°
Mean anomaly
232.8774°
Eccentric anomaly
232.85784°
Mean motion
3.80477 °/min
Orbital period
94.62 mins
BSTAR
0.00043952
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-08 21:08:18.192Z | 247.366° WSW | 2025-11-08 21:11:18.192Z | 186.648° SSW | 22.495° | 2025-11-08 21:13:18.192Z | 148.398° SSE |
| 5 mins | 2025-11-09 17:26:18.192Z | 212.796° SW | 2025-11-09 17:28:18.192Z | 164.15° S | 25.904° | 2025-11-09 17:31:18.192Z | 107.805° ESE |
| 5 mins | 2025-11-09 19:05:18.192Z | 242.215° WSW | 2025-11-09 19:07:18.192Z | 197.347° SSW | 31.266° | 2025-11-09 19:10:18.192Z | 119.426° 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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