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 25352.87372431 .00000140 00000-0 19898-3 0 9997
2 62802 88.9763 102.4669 0017951 342.3749 17.6777 13.50986161 48056Epoch: 2025-12-18T20:58Z
TLE epoch observation values (Epoch: 2025-12-18T20:58:09.780Z)
Latitude
-0.00003°
Longitude
60.20317°
Altitude
1,058.849 km
Speed
7.329 km/s
True Right ascension
06h 49m 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
05:12:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,079.046 km
Perigee altitude
1,052.321 km
Semi-major axis
7,443.821 km
Eccentricity
0.0018
Inclination
88.9763°
RAAN
102.4669°
Arg. of periapsis
342.3749°
True anomaly
17.7403°
Mean anomaly
17.6777°
Eccentric anomaly
17.70899°
Mean motion
3.37948 °/min
Orbital period
106.53 mins
BSTAR
0.00019898
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-12-19 07:44:05.237Z | 169.584° S | 2025-12-19 07:50:05.237Z | 66.942° ENE | 43.95° | 2025-12-19 07:56:05.237Z | 2.938° NNE |
| 5 mins | 2025-12-19 09:35:05.237Z | 263.392° W | 2025-12-19 09:37:05.237Z | 284.209° WNW | 15.846° | 2025-12-19 09:40:05.237Z | 314.067° NW |
| 10 mins | 2025-12-19 18:55:05.237Z | 27.396° NE | 2025-12-19 18:59:05.237Z | 78.776° E | 30.72° | 2025-12-19 19:05:05.237Z | 147.639° SSE |
| 10 mins | 2025-12-19 20:41:05.237Z | 337.556° N | 2025-12-19 20:46:05.237Z | 274.675° WNW | 30.095° | 2025-12-19 20:51:05.237Z | 220.338° SW |
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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