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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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: 6 hours ago
TLE from 6 hours ago
0 QIANFAN-1
1 60379U 24140A 26053.83093471 .00000103 00000-0 14020-3 0 9991
2 60379 88.9734 291.8277 0018120 12.2218 347.9369 13.50997633 77089Epoch: 2026-02-22T19:56Z
TLE epoch observation values (Epoch: 2026-02-22T19:56:32.758Z)
Latitude
-0.00005°
Longitude
-160.04232°
Altitude
1,058.346 km
Speed
7.329 km/s
True Right ascension
19h 27m 18s
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
04:42:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,079.13 km
Perigee altitude
1,052.153 km
Semi-major axis
7,443.778 km
Eccentricity
0.00181
Inclination
88.9734°
RAAN
291.8277°
Arg. of periapsis
12.2218°
True anomaly
347.89341°
Mean anomaly
347.9369°
Eccentric anomaly
347.91516°
Mean motion
3.3795 °/min
Orbital period
106.52 mins
BSTAR
0.0001402
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-02-23 03:38:34.311Z | 10.542° NNE | 2026-02-23 03:44:34.311Z | 88.463° E | 39.93° | 2026-02-23 03:50:34.311Z | 164.382° S |
| 7 mins | 2026-02-23 05:27:34.311Z | 318.949° NNW | 2026-02-23 05:30:34.311Z | 284.571° WNW | 21.33° | 2026-02-23 05:34:34.311Z | 242.268° WSW |
| 11 mins | 2026-02-23 15:36:34.311Z | 150.995° SSE | 2026-02-23 15:41:34.311Z | 83.959° E | 37.084° | 2026-02-23 15:47:34.311Z | 11.166° NNE |
| 9 mins | 2026-02-23 17:24:34.311Z | 235.405° WSW | 2026-02-23 17:28:34.311Z | 282.359° WNW | 23.394° | 2026-02-23 17:33:34.311Z | 333.558° NNW |
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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