QIANFAN-12, 60390
Orbit data source: Space-Track
QIANFAN-12, 60390 is a Chinese payload satellite in LEO that was launched on Tue, 06 Aug 2024 UTC via a CHANG ZHENG 6A 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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60390 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
Mission
Operational Commercial Communications
Bus & Motor
QIANFAN, Unknown motor
Mass
267 kg wet, ~267 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 5.0 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 QIANFAN-12
1 60390U 24140M 25325.85999925 .00000070 00000-0 89436-4 0 9993
2 60390 88.9721 301.4815 0011152 267.0202 92.9673 13.50975262 64428Epoch: 2025-11-21T20:38Z
TLE epoch observation values (Epoch: 2025-11-21T20:38:23.935Z)
Latitude
-0°
Longitude
-69.2152°
Altitude
1,072.065 km
Speed
7.316 km/s
True Right ascension
20h 05m 55s
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
04:19:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.025 km
Perigee altitude
1,057.422 km
Semi-major axis
7,443.861 km
Eccentricity
0.00112
Inclination
88.9721°
RAAN
301.4815°
Arg. of periapsis
267.0202°
True anomaly
93.09491°
Mean anomaly
92.9673°
Eccentric anomaly
93.03111°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.000089436
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Other satellites on launch #140 in the year 2024 (2024-08-06 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.QIANFAN-12 Visibility forecast
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-11-22 09:41:29.322Z | 28.754° NE | 2025-11-22 09:46:29.322Z | 84.174° E | 24.36° | 2025-11-22 09:51:29.322Z | 135.213° SSE |
| 10 mins | 2025-11-22 11:28:29.322Z | 342.599° N | 2025-11-22 11:32:29.322Z | 290.916° WNW | 36.145° | 2025-11-22 11:38:29.322Z | 208.792° SW |
| 8 mins | 2025-11-22 21:40:29.322Z | 114.641° SE | 2025-11-22 21:43:29.322Z | 81.895° E | 21.78° | 2025-11-22 21:48:29.322Z | 28.916° NE |
| 11 mins | 2025-11-22 23:25:29.322Z | 202.043° SSW | 2025-11-22 23:30:29.322Z | 288.696° WNW | 38.867° | 2025-11-22 23:36:29.322Z | 350.129° N |
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
Authenticating...
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