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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-1
1 60379U 24140A 26171.44293580 .00000123 00000-0 17193-3 0 9998
2 60379 88.9737 279.5917 0018130 34.2000 326.0315 13.51015389 92963Epoch: 2026-06-20T10:37Z
TLE epoch observation values (Epoch: 2026-06-20T10:37:49.653Z)
Latitude
-0°
Longitude
-148.52268°
Altitude
1,060.287 km
Speed
7.327 km/s
True Right ascension
18h 38m 22s
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
07:23:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,079.072 km
Perigee altitude
1,052.081 km
Semi-major axis
7,443.713 km
Eccentricity
0.00181
Inclination
88.9737°
RAAN
279.5917°
Arg. of periapsis
34.2°
True anomaly
325.9152°
Mean anomaly
326.0315°
Eccentric anomaly
325.97337°
Mean motion
3.37955 °/min
Orbital period
106.52 mins
BSTAR
0.00017193
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-21 06:19:11.679Z | 118.345° SE | 2026-06-21 06:23:11.679Z | 77.524° E | 20.35° | 2026-06-21 06:27:11.679Z | 34.487° NE |
| 11 mins | 2026-06-21 08:04:11.679Z | 196.66° SSW | 2026-06-21 08:09:11.679Z | 264.904° W | 40.3° | 2026-06-21 08:15:11.679Z | 349.739° N |
| 11 mins | 2026-06-21 19:14:11.679Z | 9.176° NNE | 2026-06-21 19:19:11.679Z | 107.031° ESE | 42.948° | 2026-06-21 19:25:11.679Z | 172.391° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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