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: 6 hours ago
TLE from 6 hours ago
0 GAOFEN 11-05
1 60249U 24130A 25261.01150067 .00006570 00000-0 27927-3 0 9995
2 60249 97.4282 337.6242 0001607 43.5121 316.6242 15.23372919 44028Epoch: 2025-09-18T00:16Z
TLE epoch observation values (Epoch: 2025-09-18T00:16:33.657Z)
Latitude
-0.0001°
Longitude
-23.69525°
Altitude
497.967 km
Speed
7.616 km/s
True Right ascension
22h 30m 29s
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
22:55:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.742 km
Perigee altitude
491.534 km
Semi-major axis
6,870.775 km
Eccentricity
0.00016
Inclination
97.4282°
RAAN
337.6242°
Arg. of periapsis
43.5121°
True anomaly
316.61155°
Mean anomaly
316.6242°
Eccentric anomaly
316.61788°
Mean motion
3.81096 °/min
Orbital period
94.46 mins
BSTAR
0.00027927
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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 | 2025-09-18 18:10:16.745Z | 7.677° NNE | 2025-09-18 18:13:16.745Z | 330.003° NNW | 42.633° | 2025-09-18 18:16:16.745Z | 200.524° SSW |
| 5 mins | 2025-09-19 04:48:16.745Z | 125.966° SE | 2025-09-19 04:50:16.745Z | 62.775° ENE | 30.962° | 2025-09-19 04:53:16.745Z | 5.578° NNE |
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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