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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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, 1.2 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-72
1 62802U 25016T 26141.92557832 .00000090 00000-0 12138-3 0 9994
2 62802 88.9711 86.4553 0016661 252.2649 107.6684 13.51011414 68855Epoch: 2026-05-21T22:12Z
TLE epoch observation values (Epoch: 2026-05-21T22:12:49.966Z)
Latitude
-0.00003°
Longitude
-126.31668°
Altitude
1,075.278 km
Speed
7.313 km/s
True Right ascension
05h 45m 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
15:38:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.993 km
Perigee altitude
1,053.189 km
Semi-major axis
7,443.728 km
Eccentricity
0.00167
Inclination
88.9711°
RAAN
86.4553°
Arg. of periapsis
252.2649°
True anomaly
107.8502°
Mean anomaly
107.6684°
Eccentric anomaly
107.75931°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.00012138
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-05-22 07:42:26.172Z | 23.077° NE | 2026-05-22 07:47:26.172Z | 81.564° E | 29.669° | 2026-05-22 07:52:26.172Z | 141.904° SSE |
| 10 mins | 2026-05-22 09:29:26.172Z | 337.713° N | 2026-05-22 09:34:26.172Z | 271.597° WNW | 30.843° | 2026-05-22 09:39:26.172Z | 218.127° SW |
| 10 mins | 2026-05-22 19:40:26.172Z | 129.702° SE | 2026-05-22 19:44:26.172Z | 85.216° E | 26.798° | 2026-05-22 19:50:26.172Z | 20.238° NNE |
| 11 mins | 2026-05-22 21:26:26.172Z | 211.67° SW | 2026-05-22 21:31:26.172Z | 281.131° WNW | 33.975° | 2026-05-22 21:37:26.172Z | 345.383° 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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