QIANFAN-72, 62802
Orbit data source: Space-Track
QIANFAN-72, 62802 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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62802 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: 18 hours ago
TLE from 18 hours ago
0 QIANFAN-72
1 62802U 25016T 25259.60988188 .00000064 00000-0 82089-4 0 9994
2 62802 88.9752 112.1171 0017507 246.1320 113.7996 13.49485012 35462Epoch: 2025-09-16T14:38Z
TLE epoch observation values (Epoch: 2025-09-16T14:38:13.794Z)
Latitude
-0.00001°
Longitude
-103.23809°
Altitude
1,082.39 km
Speed
7.308 km/s
True Right ascension
07h 28m 28s
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
01:25:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,084.249 km
Perigee altitude
1,058.166 km
Semi-major axis
7,449.344 km
Eccentricity
0.00175
Inclination
88.9752°
RAAN
112.1171°
Arg. of periapsis
246.132°
True anomaly
113.98299°
Mean anomaly
113.7996°
Eccentric anomaly
113.89131°
Mean motion
3.37572 °/min
Orbital period
106.64 mins
BSTAR
0.000082089
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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-72 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-09-17 13:52:57.276Z | 144.583° SSE | 2025-09-17 13:57:57.276Z | 89.067° E | 32.898° | 2025-09-17 14:03:57.276Z | 15.872° NNE |
| 9 mins | 2025-09-17 15:40:57.276Z | 226.772° WSW | 2025-09-17 15:44:57.276Z | 276.466° WNW | 27.997° | 2025-09-17 15:49:57.276Z | 334.514° NNW |
| 7 mins | 2025-09-18 01:04:57.276Z | 44.802° NE | 2025-09-18 01:07:57.276Z | 76.577° E | 18.588° | 2025-09-18 01:11:57.276Z | 117.006° SE |
| 11 mins | 2025-09-18 02:49:57.276Z | 352.58° N | 2025-09-18 02:54:57.276Z | 287.532° WNW | 42.157° | 2025-09-18 03:00:57.276Z | 196.299° SSW |
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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