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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-67
1 62797U 25016N 25352.54056159 .00000138 00000-0 19460-3 0 9992
2 62797 88.9776 102.4561 0013762 333.7261 26.3191 13.50982915 48042Epoch: 2025-12-18T12:58Z
TLE epoch observation values (Epoch: 2025-12-18T12:58:24.521Z)
Latitude
0.00003°
Longitude
-179.54067°
Altitude
1,062.413 km
Speed
7.325 km/s
True Right ascension
06h 49m 49s
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
21:01:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.94 km
Perigee altitude
1,055.451 km
Semi-major axis
7,443.833 km
Eccentricity
0.00138
Inclination
88.9776°
RAAN
102.4561°
Arg. of periapsis
333.7261°
True anomaly
26.38913°
Mean anomaly
26.3191°
Eccentric anomaly
26.3541°
Mean motion
3.37947 °/min
Orbital period
106.53 mins
BSTAR
0.0001946
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-12-19 06:52:17.380Z | 131.671° SE | 2025-12-19 06:57:17.380Z | 75.507° E | 26.36° | 2025-12-19 07:02:17.380Z | 22.415° NNE |
| 11 mins | 2025-12-19 08:38:17.380Z | 208.913° SW | 2025-12-19 08:43:17.380Z | 271.849° WNW | 34.259° | 2025-12-19 08:49:17.380Z | 344.311° N |
| 4 mins | 2025-12-19 18:04:17.380Z | 61.647° ENE | 2025-12-19 18:05:17.380Z | 71.305° E | 13.379° | 2025-12-19 18:08:17.380Z | 99.333° ESE |
| 11 mins | 2025-12-19 19:48:17.380Z | 0.44° NNE | 2025-12-19 19:53:17.380Z | 195.207° SSW | 44.754° | 2025-12-19 19:59:17.380Z | 183.639° SSW |
| 4 mins | 2025-12-19 21:37:17.380Z | 301.202° NW | 2025-12-19 21:38:17.380Z | 291.645° WNW | 13.009° | 2025-12-19 21:41:17.380Z | 264.236° W |
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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