QIANFAN-118, 68645
Orbit data source: Space-Track
QIANFAN-118, 68645 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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68645 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, 2.3 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-118
1 68645U 26075K 26171.30315707 .00000096 00000-0 12979-3 0 9998
2 68645 88.9896 320.6867 0002087 93.6069 266.5321 13.51019370 10221Epoch: 2026-06-20T07:16Z
TLE epoch observation values (Epoch: 2026-06-20T07:16:32.770Z)
Latitude
-0.00003°
Longitude
-56.96956°
Altitude
1,071.558 km
Speed
7.316 km/s
True Right ascension
21h 22m 44s
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
07:12:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,067.115 km
Perigee altitude
1,064.008 km
Semi-major axis
7,443.698 km
Eccentricity
0.00021
Inclination
88.9896°
RAAN
320.6867°
Arg. of periapsis
93.6069°
True anomaly
266.50823°
Mean anomaly
266.5321°
Eccentric anomaly
266.52016°
Mean motion
3.37956 °/min
Orbital period
106.52 mins
BSTAR
0.00012979
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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-118 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 22:05:04.066Z | 4.922° NNE | 2026-06-20 22:11:04.066Z | 78.523° E | 43.888° | 2026-06-20 22:17:04.066Z | 174.558° S |
| 6 mins | 2026-06-20 23:54:04.066Z | 316.439° NNW | 2026-06-20 23:57:04.066Z | 286.108° WNW | 16.412° | 2026-06-21 00:00:04.066Z | 256.417° W |
| 11 mins | 2026-06-21 10:03:04.066Z | 162.308° S | 2026-06-21 10:08:04.066Z | 89.156° E | 42.218° | 2026-06-21 10:14:04.066Z | 6.16° NNE |
| 7 mins | 2026-06-21 11:52:04.066Z | 249.321° W | 2026-06-21 11:55:04.066Z | 281.013° WNW | 18.463° | 2026-06-21 11:59:04.066Z | 321.829° 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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