GAOFEN 11-05, 60249
Orbit data source: Space-Track
GAOFEN 11-05, 60249 is a payload satellite owned by Yaogan Zongti (CN) in SSO that was launched on Fri, 19 Jul 2024 UTC via a CHANG ZHENG 4B launch vehicle from the Taiyaun Space Center, China (TSC). 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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60249 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST/YWZB
Mission
Operational Defense Imaging
Bus & Motor
JB-16, Unknown motor
Mass
~3,000 kg wet, ~3,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 4.0 m
Radar Cross Section
9.231 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 GAOFEN 11-05
1 60249U 24130A 25351.64749219 .00005755 00000-0 24501-3 0 9996
2 60249 97.4199 67.2850 0005419 3.5875 356.5399 15.23367179 57823Epoch: 2025-12-17T15:32Z
TLE epoch observation values (Epoch: 2025-12-17T15:32:23.325Z)
Latitude
-0.00009°
Longitude
107.67348°
Altitude
495.068 km
Speed
7.619 km/s
True Right ascension
04h 29m 08s
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
00:30:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.378 km
Perigee altitude
488.932 km
Semi-major axis
6,870.792 km
Eccentricity
0.00054
Inclination
97.4199°
RAAN
67.285°
Arg. of periapsis
3.5875°
True anomaly
356.53615°
Mean anomaly
356.5399°
Eccentric anomaly
356.53803°
Mean motion
3.81095 °/min
Orbital period
94.46 mins
BSTAR
0.00024501
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Other satellites on launch #130 in the year 2024 (2024-07-19 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.GAOFEN 11-05 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 | 2025-12-18 04:18:30.905Z | 103.606° ESE | 2025-12-18 04:20:30.905Z | 67.85° E | 15.55° | 2025-12-18 04:22:30.905Z | 32.203° NE |
| 4 mins | 2025-12-18 05:52:30.905Z | 223.895° SW | 2025-12-18 05:53:30.905Z | 249.74° W | 25.301° | 2025-12-18 05:56:30.905Z | 319.605° NNW |
| 4 mins | 2025-12-18 17:21:30.905Z | 65.506° ENE | 2025-12-18 17:22:30.905Z | 87.996° E | 20.304° | 2025-12-18 17:25:30.905Z | 145.999° 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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