QIANFAN-66, 62796
Orbit data source: Space-Track
QIANFAN-66, 62796 is a Chinese payload satellite in LEO that was launched on Thu, 23 Jan 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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62796 intel report (Beta)
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Edit Public Description
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, 1.3 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 QIANFAN-66
1 62796U 25016M 26035.82606481 .00000123 00000-0 17138-3 0 9994
2 62796 88.9740 97.4457 0015637 175.2531 184.8771 13.50993915 54594Epoch: 2026-02-04T19:49Z
TLE epoch observation values (Epoch: 2026-02-04T19:49:31.999Z)
Latitude
-0.00006°
Longitude
25.07529°
Altitude
1,083.162 km
Speed
7.305 km/s
True Right ascension
06h 29m 46s
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
03:18:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.295 km
Perigee altitude
1,054.015 km
Semi-major axis
7,443.792 km
Eccentricity
0.00156
Inclination
88.974°
RAAN
97.4457°
Arg. of periapsis
175.2531°
True anomaly
184.8619°
Mean anomaly
184.8771°
Eccentric anomaly
184.86949°
Mean motion
3.3795 °/min
Orbital period
106.52 mins
BSTAR
0.00017138
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Other satellites on launch #16 in the year 2025 (2025-01-23 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-66 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-02-05 03:04:24.634Z | 117.142° SE | 2026-02-05 03:08:24.634Z | 77.814° E | 19.717° | 2026-02-05 03:12:24.634Z | 35.677° NE |
| 11 mins | 2026-02-05 04:49:24.634Z | 194.392° SSW | 2026-02-05 04:54:24.634Z | 262.569° W | 41.36° | 2026-02-05 05:00:24.634Z | 350.699° N |
| 11 mins | 2026-02-05 15:59:24.634Z | 10.408° NNE | 2026-02-05 16:04:24.634Z | 100.152° ESE | 42.233° | 2026-02-05 16:10:24.634Z | 170.317° S |
| 7 mins | 2026-02-05 17:47:24.634Z | 315.045° NNW | 2026-02-05 17:50:24.634Z | 282.122° WNW | 18.309° | 2026-02-05 17:54:24.634Z | 243.947° WSW |
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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