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: 6 hours ago
TLE from 6 hours ago
0 QIANFAN-72
1 62802U 25016T 25310.73116207 .00000051 00000-0 59270-4 0 9993
2 62802 88.9730 106.8247 0020692 99.6309 260.7181 13.50974622 42367Epoch: 2025-11-06T17:32Z
TLE epoch observation values (Epoch: 2025-11-06T17:32:52.402Z)
Latitude
-0.00005°
Longitude
157.42108°
Altitude
1,074.145 km
Speed
7.314 km/s
True Right ascension
07h 07m 17s
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
19:28:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,081.129 km
Perigee altitude
1,050.323 km
Semi-major axis
7,443.863 km
Eccentricity
0.00207
Inclination
88.973°
RAAN
106.8247°
Arg. of periapsis
99.6309°
True anomaly
260.48419°
Mean anomaly
260.7181°
Eccentric anomaly
260.60114°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.00005927
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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 | 2025-11-06 23:28:39.155Z | 346.879° N | 2025-11-06 23:33:39.155Z | 287.843° WNW | 36.712° | 2025-11-06 23:39:39.155Z | 207.247° SW |
| 8 mins | 2025-11-07 09:41:39.155Z | 114.356° SE | 2025-11-07 09:45:39.155Z | 69.061° E | 21.058° | 2025-11-07 09:49:39.155Z | 29.32° NE |
| 10 mins | 2025-11-07 11:26:39.155Z | 200.771° SSW | 2025-11-07 11:31:39.155Z | 288.62° WNW | 39.255° | 2025-11-07 11:36:39.155Z | 347.849° N |
| 11 mins | 2025-11-07 22:35:39.155Z | 7.322° NNE | 2025-11-07 22:40:39.155Z | 87.669° E | 43.577° | 2025-11-07 22:46:39.155Z | 173.483° S |
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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