QIANFAN-92, 66034
Orbit data source: Space-Track
QIANFAN-92, 66034 is a Chinese payload satellite in LEO that was launched on Fri, 17 Oct 2025 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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66034 intel report (Beta)
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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, 14.5 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-92
1 66034U 25233B 26177.69549727 .00000108 00000-0 14800-3 0 9991
2 66034 88.9979 42.1997 0001958 80.5841 279.5531 13.51015972 34465Epoch: 2026-06-26T16:41Z
TLE epoch observation values (Epoch: 2026-06-26T16:41:30.964Z)
Latitude
-0.00005°
Longitude
-122.99963°
Altitude
1,071.234 km
Speed
7.316 km/s
True Right ascension
02h 48m 47s
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
12:10:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,067.031 km
Perigee altitude
1,064.116 km
Semi-major axis
7,443.711 km
Eccentricity
0.0002
Inclination
88.9979°
RAAN
42.1997°
Arg. of periapsis
80.5841°
True anomaly
279.53097°
Mean anomaly
279.5531°
Eccentric anomaly
279.54204°
Mean motion
3.37955 °/min
Orbital period
106.52 mins
BSTAR
0.000148
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Other satellites on launch #233 in the year 2025 (2025-10-17 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-92 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-06-27 02:10:56.914Z | 26.858° NE | 2026-06-27 02:15:56.914Z | 80.493° E | 24.662° | 2026-06-27 02:20:56.914Z | 134.291° SE |
| 10 mins | 2026-06-27 03:57:56.914Z | 343.405° N | 2026-06-27 04:02:56.914Z | 270.903° WNW | 35.968° | 2026-06-27 04:07:56.914Z | 210.329° SW |
| 8 mins | 2026-06-27 14:09:56.914Z | 117.53° SE | 2026-06-27 14:13:56.914Z | 72.498° E | 22.177° | 2026-06-27 14:17:56.914Z | 30.471° NE |
| 11 mins | 2026-06-27 15:54:56.914Z | 201.651° SSW | 2026-06-27 15:59:56.914Z | 278.822° WNW | 38.732° | 2026-06-27 16:05:56.914Z | 348.997° 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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