QIANFAN-102, 66044
Orbit data source: Space-Track
QIANFAN-102, 66044 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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66044 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
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-102
1 66044U 25233M 26130.18430236 .00000124 00000-0 17379-3 0 9991
2 66044 89.0024 46.9365 0002197 72.6000 287.5391 13.51016202 28109Epoch: 2026-05-10T04:25Z
TLE epoch observation values (Epoch: 2026-05-10T04:25:23.723Z)
Latitude
-0.00007°
Longitude
112.59663°
Altitude
1,070.983 km
Speed
7.317 km/s
True Right ascension
03h 07m 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
19:44:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,067.208 km
Perigee altitude
1,063.938 km
Semi-major axis
7,443.71 km
Eccentricity
0.00022
Inclination
89.0024°
RAAN
46.9365°
Arg. of periapsis
72.6°
True anomaly
287.51509°
Mean anomaly
287.5391°
Eccentric anomaly
287.5271°
Mean motion
3.37955 °/min
Orbital period
106.52 mins
BSTAR
0.00017379
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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-102 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 | 2026-05-10 18:45:28.794Z | 172.07° S | 2026-05-10 18:50:28.794Z | 75.011° E | 44.65° | 2026-05-10 18:56:28.794Z | 1.467° NNE |
| 5 mins | 2026-05-10 20:35:28.794Z | 262.973° W | 2026-05-10 20:37:28.794Z | 282.712° WNW | 14.645° | 2026-05-10 20:40:28.794Z | 311.912° NW |
| 10 mins | 2026-05-11 05:55:28.794Z | 25.009° NE | 2026-05-11 05:59:28.794Z | 76.461° E | 32.043° | 2026-05-11 06:05:28.794Z | 149.77° SSE |
| 9 mins | 2026-05-11 07:42:28.794Z | 330.122° NNW | 2026-05-11 07:46:28.794Z | 276.649° WNW | 28.366° | 2026-05-11 07:51:28.794Z | 222.994° SW |
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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