QIANFAN-114, 68641
Orbit data source: Space-Track
QIANFAN-114, 68641 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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68641 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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-114
1 68641U 26075F 26171.41425080 .00000077 00000-0 10004-3 0 9998
2 68641 88.9893 320.6843 0002008 96.2165 263.9215 13.51013570 10237Epoch: 2026-06-20T09:56Z
TLE epoch observation values (Epoch: 2026-06-20T09:56:31.269Z)
Latitude
0°
Longitude
-97.0752°
Altitude
1,071.644 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
07:11:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,067.077 km
Perigee altitude
1,064.088 km
Semi-major axis
7,443.72 km
Eccentricity
0.0002
Inclination
88.9893°
RAAN
320.6843°
Arg. of periapsis
96.2165°
True anomaly
263.89862°
Mean anomaly
263.9215°
Eccentric anomaly
263.91006°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.00010004
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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-114 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-06-20 21:12:05.431Z | 23.037° NE | 2026-06-20 21:18:05.431Z | 88.107° E | 25.672° | 2026-06-20 21:23:05.431Z | 138.724° SSE |
| 10 mins | 2026-06-20 23:00:05.431Z | 339.481° N | 2026-06-20 23:04:05.431Z | 283.888° WNW | 34.775° | 2026-06-20 23:10:05.431Z | 210.563° SW |
| 8 mins | 2026-06-21 09:12:05.431Z | 114.918° SE | 2026-06-21 09:15:05.431Z | 79.55° E | 23.267° | 2026-06-21 09:20:05.431Z | 26.447° NE |
| 11 mins | 2026-06-21 10:56:05.431Z | 201.957° SSW | 2026-06-21 11:01:05.431Z | 263.172° W | 37.44° | 2026-06-21 11:07:05.431Z | 346.322° N |
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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