QIANFAN-62, 62792
Orbit data source: Space-Track
QIANFAN-62, 62792 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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62792 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, 5.0 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-62
1 62792U 25016H 25256.90240609 .00000052 00000-0 62779-4 0 9992
2 62792 88.9770 112.3959 0014346 241.0138 118.9576 13.50964889 35103Epoch: 2025-09-13T21:39Z
TLE epoch observation values (Epoch: 2025-09-13T21:39:27.886Z)
Latitude
0.00004°
Longitude
154.40061°
Altitude
1,076.849 km
Speed
7.311 km/s
True Right ascension
07h 29m 35s
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
00:19:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.441 km
Perigee altitude
1,055.083 km
Semi-major axis
7,443.899 km
Eccentricity
0.00143
Inclination
88.977°
RAAN
112.3959°
Arg. of periapsis
241.0138°
True anomaly
119.10132°
Mean anomaly
118.9576°
Eccentric anomaly
119.02947°
Mean motion
3.37942 °/min
Orbital period
106.53 mins
BSTAR
0.000062779
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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-62 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 | 2025-09-14 13:46:43.740Z | 130.394° SE | 2025-09-14 13:51:43.740Z | 76.097° E | 25.646° | 2025-09-14 13:56:43.740Z | 23.439° NE |
| 11 mins | 2025-09-14 15:32:43.740Z | 207.112° SW | 2025-09-14 15:37:43.740Z | 270.824° WNW | 35.428° | 2025-09-14 15:43:43.740Z | 344.978° N |
| 4 mins | 2025-09-15 00:58:43.740Z | 61.217° ENE | 2025-09-15 00:59:43.740Z | 70.677° E | 12.55° | 2025-09-15 01:02:43.740Z | 98.223° ESE |
| 11 mins | 2025-09-15 02:42:43.740Z | 1.77° NNE | 2025-09-15 02:47:43.740Z | 164.295° S | 44.843° | 2025-09-15 02:53:43.740Z | 181.896° SSW |
| 4 mins | 2025-09-15 04:31:43.740Z | 302.168° NW | 2025-09-15 04:32:43.740Z | 292.43° WNW | 13.543° | 2025-09-15 04:35:43.740Z | 264.203° W |
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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