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 25357.28066171 .00000170 00000-0 24450-3 0 9994
2 62797 88.9775 101.9671 0013464 318.6312 41.3818 13.50984374 48689Epoch: 2025-12-23T06:44Z
TLE epoch observation values (Epoch: 2025-12-23T06:44:09.171Z)
Latitude
-0.00009°
Longitude
-91.13778°
Altitude
1,064.074 km
Speed
7.324 km/s
True Right ascension
06h 47m 52s
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
14:30:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.713 km
Perigee altitude
1,055.668 km
Semi-major axis
7,443.827 km
Eccentricity
0.00135
Inclination
88.9775°
RAAN
101.9671°
Arg. of periapsis
318.6312°
True anomaly
41.48392°
Mean anomaly
41.3818°
Eccentric anomaly
41.43285°
Mean motion
3.37947 °/min
Orbital period
106.53 mins
BSTAR
0.0002445
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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 | 2025-12-23 18:01:01.432Z | 37.117° NE | 2025-12-23 18:05:01.432Z | 76.592° E | 18.165° | 2025-12-23 18:09:01.432Z | 116.435° SE |
| 11 mins | 2025-12-23 19:47:01.432Z | 353.014° N | 2025-12-23 19:52:01.432Z | 282.184° WNW | 42.649° | 2025-12-23 19:58:01.432Z | 195.056° SSW |
| 6 mins | 2025-12-24 06:01:01.432Z | 95.881° ESE | 2025-12-24 06:03:01.432Z | 75.654° E | 15.881° | 2025-12-24 06:07:01.432Z | 37.295° NE |
| 11 mins | 2025-12-24 07:44:01.432Z | 185.311° SSW | 2025-12-24 07:49:01.432Z | 266.789° W | 44.215° | 2025-12-24 07:55:01.432Z | 355.498° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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