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: 1 day ago
TLE from 1 day ago
0 QIANFAN-67
1 62797U 25016N 25306.47245300 .00000078 00000-0 10111-3 0 9998
2 62797 88.9739 107.2148 0016691 101.4581 258.8446 13.50971033 41827Epoch: 2025-11-02T11:20Z
TLE epoch observation values (Epoch: 2025-11-02T11:20:19.939Z)
Latitude
0.00002°
Longitude
-104.85597°
Altitude
1,074.066 km
Speed
7.314 km/s
True Right ascension
07h 08m 51s
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
14:39:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.164 km
Perigee altitude
1,053.315 km
Semi-major axis
7,443.876 km
Eccentricity
0.00167
Inclination
88.9739°
RAAN
107.2148°
Arg. of periapsis
101.4581°
True anomaly
258.65703°
Mean anomaly
258.8446°
Eccentric anomaly
258.7508°
Mean motion
3.37944 °/min
Orbital period
106.53 mins
BSTAR
0.00010111
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-03 21:43:48.351Z | 37.353° NE | 2025-11-03 21:47:48.351Z | 79.428° E | 19.522° | 2025-11-03 21:51:48.351Z | 120.414° SE |
| 11 mins | 2025-11-03 23:29:48.351Z | 350.087° N | 2025-11-03 23:34:48.351Z | 270.337° WNW | 41.081° | 2025-11-03 23:40:48.351Z | 198.119° SSW |
| 7 mins | 2025-11-04 09:42:48.351Z | 105.338° ESE | 2025-11-04 09:45:48.351Z | 74.705° E | 17.416° | 2025-11-04 09:49:48.351Z | 35.318° NE |
| 11 mins | 2025-11-04 11:26:48.351Z | 189.827° SSW | 2025-11-04 11:31:48.351Z | 274.274° WNW | 43.143° | 2025-11-04 11:37:48.351Z | 353.688° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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