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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-102
1 66044U 25233M 26177.58442795 .00000107 00000-0 14763-3 0 9994
2 66044 88.9998 42.1528 0002015 85.2478 274.8903 13.51013301 34500Epoch: 2026-06-26T14:01Z
TLE epoch observation values (Epoch: 2026-06-26T14:01:34.574Z)
Latitude
-0.00007°
Longitude
-82.9521°
Altitude
1,071.358 km
Speed
7.316 km/s
True Right ascension
02h 48m 36s
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
10:53:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,067.084 km
Perigee altitude
1,064.084 km
Semi-major axis
7,443.721 km
Eccentricity
0.0002
Inclination
88.9998°
RAAN
42.1528°
Arg. of periapsis
85.2478°
True anomaly
274.86729°
Mean anomaly
274.8903°
Eccentric anomaly
274.8788°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.00014763
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-06-27 03:03:44.859Z | 6.458° NNE | 2026-06-27 03:09:44.859Z | 100.194° ESE | 43.277° | 2026-06-27 03:15:44.859Z | 172.905° S |
| 6 mins | 2026-06-27 04:52:44.859Z | 314.52° NW | 2026-06-27 04:55:44.859Z | 282.792° WNW | 17.245° | 2026-06-27 04:58:44.859Z | 253.126° W |
| 11 mins | 2026-06-27 15:01:44.859Z | 159.296° S | 2026-06-27 15:06:44.859Z | 75.736° E | 41.321° | 2026-06-27 15:12:44.859Z | 6.677° NNE |
| 7 mins | 2026-06-27 16:50:44.859Z | 250.896° W | 2026-06-27 16:53:44.859Z | 284.472° WNW | 19.384° | 2026-06-27 16:57:44.859Z | 324.725° 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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