QIANFAN-1, 60379
Orbit data source: Space-Track
QIANFAN-1, 60379 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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60379 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: 13 hours ago
TLE from 13 hours ago
0 QIANFAN-1
1 60379U 24140A 25261.22218405 .00000073 00000-0 94530-4 0 9991
2 60379 88.9785 308.1438 0019747 101.8440 258.4927 13.50972641 55808Epoch: 2025-09-18T05:19Z
TLE epoch observation values (Epoch: 2025-09-18T05:19:56.701Z)
Latitude
-0.00006°
Longitude
-129.22933°
Altitude
1,074.597 km
Speed
7.313 km/s
True Right ascension
20h 32m 34s
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
11:19:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,080.433 km
Perigee altitude
1,051.034 km
Semi-major axis
7,443.87 km
Eccentricity
0.00197
Inclination
88.9785°
RAAN
308.1438°
Arg. of periapsis
101.844°
True anomaly
258.27107°
Mean anomaly
258.4927°
Eccentric anomaly
258.38188°
Mean motion
3.37944 °/min
Orbital period
106.53 mins
BSTAR
0.00009453
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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-1 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-09-19 02:46:19.719Z | 142.581° SSE | 2025-09-19 02:52:19.719Z | 70.882° E | 30.777° | 2025-09-19 02:57:19.719Z | 17.626° NNE |
| 9 mins | 2025-09-19 04:34:19.719Z | 223.916° SW | 2025-09-19 04:38:19.719Z | 276.397° WNW | 29.365° | 2025-09-19 04:43:19.719Z | 336.308° NNW |
| 6 mins | 2025-09-19 13:58:19.719Z | 53.258° ENE | 2025-09-19 14:00:19.719Z | 74.379° E | 16.567° | 2025-09-19 14:04:19.719Z | 113.648° SE |
| 11 mins | 2025-09-19 15:42:19.719Z | 355.112° N | 2025-09-19 15:47:19.719Z | 297.595° NW | 43.271° | 2025-09-19 15:53:19.719Z | 192.511° SSW |
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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