QIANFAN-67, 62797
Orbit data source: Space-Track
QIANFAN-67, 62797 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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62797 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: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-67
1 62797U 25016N 25326.09960402 .00000113 00000-0 15567-3 0 9995
2 62797 88.9757 105.1853 0016025 50.3250 309.9312 13.50975064 44475Epoch: 2025-11-22T02:23Z
TLE epoch observation values (Epoch: 2025-11-22T02:23:25.787Z)
Latitude
0.00002°
Longitude
7.99472°
Altitude
1,063.976 km
Speed
7.324 km/s
True Right ascension
07h 00m 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
06:23:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.653 km
Perigee altitude
1,053.796 km
Semi-major axis
7,443.861 km
Eccentricity
0.0016
Inclination
88.9757°
RAAN
105.1853°
Arg. of periapsis
50.325°
True anomaly
309.79021°
Mean anomaly
309.9312°
Eccentric anomaly
309.86072°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.00015567
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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-67 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 | 2025-11-22 09:35:42.220Z | 166.595° S | 2025-11-22 09:41:42.220Z | 94.876° ESE | 42.983° | 2025-11-22 09:47:42.220Z | 5.075° NNE |
| 6 mins | 2025-11-22 11:26:42.220Z | 258.714° W | 2025-11-22 11:28:42.220Z | 280.146° WNW | 17.22° | 2025-11-22 11:32:42.220Z | 320.474° NNW |
| 10 mins | 2025-11-22 20:46:42.220Z | 27.452° NE | 2025-11-22 20:50:42.220Z | 74.402° E | 28.433° | 2025-11-22 20:56:42.220Z | 143.567° SSE |
| 10 mins | 2025-11-22 22:33:42.220Z | 335.151° NNW | 2025-11-22 22:37:42.220Z | 279.693° WNW | 31.983° | 2025-11-22 22:43:42.220Z | 214.321° SW |
| 9 mins | 2025-11-23 08:44:42.220Z | 125.742° SE | 2025-11-23 08:48:42.220Z | 78.268° E | 25.762° | 2025-11-23 08:53:42.220Z | 23.671° NE |
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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