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: 22 hours ago
TLE from 22 hours ago
0 YAOGAN-43 03A
1 61617U 24190A 25261.01179855 .00008021 00000-0 33370-3 0 9999
2 61617 34.9894 109.6154 0006043 7.9628 352.1182 15.23028663 50341Epoch: 2025-09-18T00:16Z
TLE epoch observation values (Epoch: 2025-09-18T00:16:59.394Z)
Latitude
-0°
Longitude
108.18841°
Altitude
491.503 km
Speed
7.624 km/s
True Right ascension
07h 18m 27s
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
14:43:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.12 km
Perigee altitude
495.807 km
Semi-major axis
6,878.1 km
Eccentricity
0.0006
Inclination
34.9894°
RAAN
109.6154°
Arg. of periapsis
7.9628°
True anomaly
352.1087°
Mean anomaly
352.1182°
Eccentric anomaly
352.11345°
Mean motion
3.80488 °/min
Orbital period
94.62 mins
BSTAR
0.0003337
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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 | 2025-09-19 17:26:31.669Z | 195.076° SSW | 2025-09-19 17:28:31.669Z | 153.544° SSE | 19.406° | 2025-09-19 17:30:31.669Z | 117.507° SE |
| 5 mins | 2025-09-19 19:05:31.669Z | 231.056° WSW | 2025-09-19 19:07:31.669Z | 177.991° S | 31.234° | 2025-09-19 19:10:31.669Z | 111.046° ESE |
| 4 mins | 2025-09-19 20:45:31.669Z | 233.165° WSW | 2025-09-19 20:47:31.669Z | 175.165° S | 27.248° | 2025-09-19 20:49:31.669Z | 134.871° 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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