QIANFAN-120, 68647
Orbit data source: Space-Track
QIANFAN-120, 68647 is a Chinese payload satellite in LEO that was launched on Tue, 07 Apr 2026 UTC via a CHANG ZHENG 8 launch vehicle from the Wenchang Satellite Launch Center (WSC). 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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68647 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
Mission
Operational spacecraft
Bus & Motor
QIANFAN, Unknown motor
Mass
267 kg wet, ~267 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 1.6 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 QIANFAN-120
1 68647U 26075M 26171.29091542 .00000081 00000-0 10755-3 0 9990
2 68647 88.9897 320.6686 0001744 108.5712 251.5629 13.51004765 10231Epoch: 2026-06-20T06:58Z
TLE epoch observation values (Epoch: 2026-06-20T06:58:55.092Z)
Latitude
0.00002°
Longitude
-52.5686°
Altitude
1,071.928 km
Speed
7.316 km/s
True Right ascension
21h 22m 40s
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
07:14:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,066.913 km
Perigee altitude
1,064.317 km
Semi-major axis
7,443.752 km
Eccentricity
0.00017
Inclination
88.9897°
RAAN
320.6686°
Arg. of periapsis
108.5712°
True anomaly
251.54394°
Mean anomaly
251.5629°
Eccentric anomaly
251.55342°
Mean motion
3.37952 °/min
Orbital period
106.52 mins
BSTAR
0.00010755
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Other satellites on launch #75 in the year 2026 (2026-04-07 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-120 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 | 2026-06-20 21:47:12.498Z | 10.158° NNE | 2026-06-20 21:53:12.498Z | 75.106° E | 38.967° | 2026-06-20 21:59:12.498Z | 162.043° S |
| 8 mins | 2026-06-20 23:36:12.498Z | 322.962° NNW | 2026-06-20 23:39:12.498Z | 289.787° WNW | 21.72° | 2026-06-20 23:44:12.498Z | 237.204° WSW |
| 10 mins | 2026-06-21 09:46:12.498Z | 146.855° SSE | 2026-06-21 09:50:12.498Z | 94.082° ESE | 36.193° | 2026-06-21 09:56:12.498Z | 12.985° NNE |
| 9 mins | 2026-06-21 11:33:12.498Z | 231.691° WSW | 2026-06-21 11:37:12.498Z | 276.865° WNW | 24.244° | 2026-06-21 11:42:12.498Z | 331.7° 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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