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 spacecraft
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
Unknown
Radar Cross Section
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 25259.63208941 .00007600 00000-0 32274-3 0 9991
2 60249 97.4280 336.2593 0001716 46.1369 314.0009 15.23354109 43814Epoch: 2025-09-16T15:10Z
TLE epoch observation values (Epoch: 2025-09-16T15:10:12.525Z)
Latitude
-0.00004°
Longitude
112.88751°
Altitude
498.007 km
Speed
7.616 km/s
True Right ascension
22h 25m 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
17:48:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.874 km
Perigee altitude
491.515 km
Semi-major axis
6,870.831 km
Eccentricity
0.00017
Inclination
97.428°
RAAN
336.2593°
Arg. of periapsis
46.1369°
True anomaly
313.98675°
Mean anomaly
314.0009°
Eccentric anomaly
313.99383°
Mean motion
3.81091 °/min
Orbital period
94.47 mins
BSTAR
0.00032274
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-17 05:28:57.012Z | 182.917° SSW | 2025-09-17 05:31:57.012Z | 262.304° W | 39.515° | 2025-09-17 05:34:57.012Z | 337.04° NNW |
| 4 mins | 2025-09-17 18:32:57.012Z | 336.526° NNW | 2025-09-17 18:34:57.012Z | 268.958° W | 30.364° | 2025-09-17 18:36:57.012Z | 225.677° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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