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, 1.2 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-72
1 62802U 25016T 25340.57910652 .00000180 00000-0 26021-3 0 9994
2 62802 88.9756 103.7370 0019042 18.7072 341.4775 13.50982295 46392Epoch: 2025-12-06T13:53Z
TLE epoch observation values (Epoch: 2025-12-06T13:53:54.803Z)
Latitude
-0°
Longitude
179.65383°
Altitude
1,058.154 km
Speed
7.329 km/s
True Right ascension
06h 54m 56s
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
20:27:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,079.872 km
Perigee altitude
1,051.523 km
Semi-major axis
7,443.835 km
Eccentricity
0.0019
Inclination
88.9756°
RAAN
103.737°
Arg. of periapsis
18.7072°
True anomaly
341.40802°
Mean anomaly
341.4775°
Eccentric anomaly
341.44278°
Mean motion
3.37947 °/min
Orbital period
106.53 mins
BSTAR
0.00026021
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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 | 2025-12-07 07:47:22.631Z | 135.502° SSE | 2025-12-07 07:52:22.631Z | 81.899° E | 27.333° | 2025-12-07 07:57:22.631Z | 23.519° NE |
| 10 mins | 2025-12-07 09:34:22.631Z | 214.095° SW | 2025-12-07 09:39:22.631Z | 285.518° WNW | 32.678° | 2025-12-07 09:44:22.631Z | 341.709° N |
| 5 mins | 2025-12-07 18:59:22.631Z | 58.189° ENE | 2025-12-07 19:01:22.631Z | 78.016° E | 14.181° | 2025-12-07 19:04:22.631Z | 105.579° ESE |
| 11 mins | 2025-12-07 20:43:22.631Z | 358.951° N | 2025-12-07 20:48:22.631Z | 274.644° WNW | 44.85° | 2025-12-07 20:54:22.631Z | 185.775° SSW |
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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