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: 5 hours ago
TLE from 5 hours ago
0 YAOGAN-43 03A
1 61617U 24190A 26279.15857005 .00005513 00000-0 22973-3 0 9994
2 61617 34.9904 219.7587 0005609 261.6496 98.3583 15.23055237108799Epoch: 2026-10-06T03:48Z
TLE epoch observation values (Epoch: 2026-10-06T03:48:20.452Z)
Latitude
0.00001°
Longitude
147.84638°
Altitude
496.1 km
Speed
7.619 km/s
True Right ascension
14h 39m 02s
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
02:19:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.741 km
Perigee altitude
496.025 km
Semi-major axis
6,878.02 km
Eccentricity
0.00056
Inclination
34.9904°
RAAN
219.7587°
Arg. of periapsis
261.6496°
True anomaly
98.42189°
Mean anomaly
98.3583°
Eccentric anomaly
98.39009°
Mean motion
3.80494 °/min
Orbital period
94.61 mins
BSTAR
0.00022973
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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 | 2026-10-07 00:31:37.795Z | 214.707° SW | 2026-10-07 00:33:37.795Z | 174.919° S | 26.955° | 2026-10-07 00:36:37.795Z | 111.847° ESE |
| 5 mins | 2026-10-07 02:11:37.795Z | 233.727° WSW | 2026-10-07 02:13:37.795Z | 171.44° S | 39.523° | 2026-10-07 02:16:37.795Z | 112.616° SE |
| 5 mins | 2026-10-07 03:50:37.795Z | 243.5° WSW | 2026-10-07 03:52:37.795Z | 202.23° SSW | 27.024° | 2026-10-07 03:55:37.795Z | 141.16° 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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