QIANFAN-2, 60380
Orbit data source: Space-Track
QIANFAN-2, 60380 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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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: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-2
1 60380U 24140B 26118.81299726 .00000054 00000-0 64399-4 0 9994
2 60380 88.9672 284.8825 0013990 145.0601 215.1471 13.51003223 85919Epoch: 2026-04-28T19:30Z
TLE epoch observation values (Epoch: 2026-04-28T19:30:42.963Z)
Latitude
-0.00002°
Longitude
135.42056°
Altitude
1,080.048 km
Speed
7.308 km/s
True Right ascension
18h 59m 31s
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
10:08:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.035 km
Perigee altitude
1,055.207 km
Semi-major axis
7,443.758 km
Eccentricity
0.0014
Inclination
88.9672°
RAAN
284.8825°
Arg. of periapsis
145.0601°
True anomaly
215.05494°
Mean anomaly
215.1471°
Eccentric anomaly
215.10101°
Mean motion
3.37952 °/min
Orbital period
106.52 mins
BSTAR
0.000064399
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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-2 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 | 2026-04-29 09:53:08.900Z | 105.615° ESE | 2026-04-29 09:57:08.900Z | 67.117° ENE | 15.553° | 2026-04-29 10:00:08.900Z | 39.048° NE |
| 11 mins | 2026-04-29 11:37:08.900Z | 184.204° SSW | 2026-04-29 11:42:08.900Z | 245.539° WSW | 44.261° | 2026-04-29 11:48:08.900Z | 355.699° N |
| 11 mins | 2026-04-29 22:47:08.900Z | 16.606° NNE | 2026-04-29 22:52:08.900Z | 94.576° ESE | 37.928° | 2026-04-29 22:58:08.900Z | 161.812° S |
| 8 mins | 2026-04-30 00:34:08.900Z | 327.087° NNW | 2026-04-30 00:38:08.900Z | 281.764° WNW | 22.668° | 2026-04-30 00:42:08.900Z | 238.458° WSW |
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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