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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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: 2 days ago
TLE from 2 days ago
0 GAOFEN 11-05
1 60249U 24130A 26135.14385824 .00002431 00000-0 10263-3 0 9998
2 60249 97.4003 213.9110 0003416 162.8145 197.3723 15.23288232 80437Epoch: 2026-05-15T03:27Z
TLE epoch observation values (Epoch: 2026-05-15T03:27:09.351Z)
Latitude
0.0513°
Longitude
-70.76399°
Altitude
501.26 km
Speed
7.613 km/s
True Right ascension
14h 15m 37s
True Declination
0° 03' 04"
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
12:16:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.239 km
Perigee altitude
490.544 km
Semi-major axis
6,871.029 km
Eccentricity
0.00034
Inclination
97.4003°
RAAN
213.911°
Arg. of periapsis
162.8145°
True anomaly
197.36062°
Mean anomaly
197.3723°
Eccentric anomaly
197.36646°
Mean motion
3.81075 °/min
Orbital period
94.47 mins
BSTAR
0.00010263
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-17 04:28:14.986Z | 116.575° SE | 2026-05-17 04:31:14.986Z | 58.326° ENE | 19.006° | 2026-05-17 04:33:14.986Z | 23.275° NE |
| 5 mins | 2026-05-17 17:31:14.986Z | 48.611° ENE | 2026-05-17 17:33:14.986Z | 97.464° ESE | 25.34° | 2026-05-17 17:36:14.986Z | 156.768° SSE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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