QIANFAN-125, 68652
Orbit data source: Space-Track
QIANFAN-125, 68652 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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68652 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: 16 hours ago
TLE from 16 hours ago
0 QIANFAN-125
1 68652U 26075S 26171.23730671 .00000076 00000-0 98792-4 0 9995
2 68652 88.9894 320.6781 0002053 94.9688 265.1697 13.51024328 10226Epoch: 2026-06-20T05:41Z
TLE epoch observation values (Epoch: 2026-06-20T05:41:43.299Z)
Latitude
-0.00009°
Longitude
-33.20713°
Altitude
1,071.575 km
Speed
7.316 km/s
True Right ascension
21h 22m 42s
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
08:33:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,067.071 km
Perigee altitude
1,064.015 km
Semi-major axis
7,443.68 km
Eccentricity
0.00021
Inclination
88.9894°
RAAN
320.6781°
Arg. of periapsis
94.9688°
True anomaly
265.14626°
Mean anomaly
265.1697°
Eccentric anomaly
265.15798°
Mean motion
3.37957 °/min
Orbital period
106.52 mins
BSTAR
0.000098792
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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-125 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 22:17:03.632Z | 0.836° NNE | 2026-06-20 22:23:03.632Z | 185.468° SSW | 44.995° | 2026-06-20 22:29:03.632Z | 182.812° SSW |
| 4 mins | 2026-06-21 00:07:03.632Z | 303.869° NW | 2026-06-21 00:08:03.632Z | 294.31° NW | 13.065° | 2026-06-21 00:11:03.632Z | 266.118° W |
| 11 mins | 2026-06-21 10:15:03.632Z | 171.187° S | 2026-06-21 10:20:03.632Z | 68.894° E | 44.503° | 2026-06-21 10:26:03.632Z | 1.822° NNE |
| 5 mins | 2026-06-21 12:05:03.632Z | 263.338° W | 2026-06-21 12:07:03.632Z | 283.348° WNW | 14.96° | 2026-06-21 12:10:03.632Z | 312.649° NW |
| 10 mins | 2026-06-21 21:25:03.632Z | 25.821° NE | 2026-06-21 21:29:03.632Z | 77.954° E | 31.727° | 2026-06-21 21:35:03.632Z | 149.482° SSE |
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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