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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-1
1 60379U 24140A 25311.80822759 .00000036 00000-0 36644-4 0 9995
2 60379 88.9729 302.9025 0016306 321.5747 38.4242 13.50978368 62636Epoch: 2025-11-07T19:23Z
TLE epoch observation values (Epoch: 2025-11-07T19:23:50.863Z)
Latitude
-0.00001°
Longitude
-35.30631°
Altitude
1,062.107 km
Speed
7.326 km/s
True Right ascension
20h 11m 36s
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
00:51:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.85 km
Perigee altitude
1,053.574 km
Semi-major axis
7,443.849 km
Eccentricity
0.00163
Inclination
88.9729°
RAAN
302.9025°
Arg. of periapsis
321.5747°
True anomaly
38.54051°
Mean anomaly
38.4242°
Eccentric anomaly
38.48234°
Mean motion
3.37946 °/min
Orbital period
106.53 mins
BSTAR
0.000036644
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-08 10:14:04.994Z | 39.517° NE | 2025-11-08 10:18:04.994Z | 76.96° E | 15.448° | 2025-11-08 10:21:04.994Z | 105.809° ESE |
| 11 mins | 2025-11-08 12:00:04.994Z | 357.101° N | 2025-11-08 12:05:04.994Z | 286.709° WNW | 44.415° | 2025-11-08 12:11:04.994Z | 188.672° SSW |
| 4 mins | 2025-11-08 22:15:04.994Z | 84.52° E | 2025-11-08 22:16:04.994Z | 74.873° E | 13.283° | 2025-11-08 22:19:04.994Z | 46.596° ENE |
| 11 mins | 2025-11-08 23:57:04.994Z | 177.959° S | 2025-11-09 00:02:04.994Z | 291.55° WNW | 44.995° | 2025-11-09 00:08:04.994Z | 358.914° N |
| 4 mins | 2025-11-09 01:48:04.994Z | 272.75° WNW | 2025-11-09 01:49:04.994Z | 282.228° WNW | 12.62° | 2025-11-09 01:52:04.994Z | 310.064° NW |
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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