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 25259.96298105 .00008592 00000-0 35750-3 0 9997
2 61617 34.9901 116.2110 0006149 357.6936 2.3750 15.23012129 50187Epoch: 2025-09-16T23:06Z
TLE epoch observation values (Epoch: 2025-09-16T23:06:41.562Z)
Latitude
0.00001°
Longitude
133.39209°
Altitude
491.444 km
Speed
7.624 km/s
True Right ascension
07h 44m 50s
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
14:08:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.242 km
Perigee altitude
495.783 km
Semi-major axis
6,878.15 km
Eccentricity
0.00061
Inclination
34.9901°
RAAN
116.211°
Arg. of periapsis
357.6936°
True anomaly
2.37792°
Mean anomaly
2.375°
Eccentric anomaly
2.37646°
Mean motion
3.80483 °/min
Orbital period
94.62 mins
BSTAR
0.0003575
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-17 21:31:42.275Z | 252.204° W | 2025-09-17 21:34:42.275Z | 193.897° SSW | 28.953° | 2025-09-17 21:37:42.275Z | 128.319° SE |
| 4 mins | 2025-09-18 17:50:42.275Z | 188.977° SSW | 2025-09-18 17:51:42.275Z | 169.17° S | 18.586° | 2025-09-18 17:54:42.275Z | 114.458° SE |
| 5 mins | 2025-09-18 19:29:42.275Z | 225.799° WSW | 2025-09-18 19:31:42.275Z | 165.631° S | 30.788° | 2025-09-18 19:34:42.275Z | 108.605° ESE |
| 5 mins | 2025-09-18 21:08:42.275Z | 243.953° WSW | 2025-09-18 21:10:42.275Z | 198.651° SSW | 28.286° | 2025-09-18 21:13:42.275Z | 130.673° 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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