QIANFAN-70, 62800
Orbit data source: Space-Track
QIANFAN-70, 62800 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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62800 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, 1.3 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-70
1 62800U 25016R 25340.64082399 .00000192 00000-0 27938-3 0 9999
2 62800 88.9772 103.7368 0014885 359.1024 1.0098 13.50975178 46416Epoch: 2025-12-06T15:22Z
TLE epoch observation values (Epoch: 2025-12-06T15:22:47.192Z)
Latitude
-0.00002°
Longitude
157.37451°
Altitude
1,060.541 km
Speed
7.327 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
21:38:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.804 km
Perigee altitude
1,054.644 km
Semi-major axis
7,443.861 km
Eccentricity
0.00149
Inclination
88.9772°
RAAN
103.7368°
Arg. of periapsis
359.1024°
True anomaly
1.01281°
Mean anomaly
1.0098°
Eccentric anomaly
1.01131°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.00027938
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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-70 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-12-07 07:30:38.332Z | 121.057° SE | 2025-12-07 07:34:38.332Z | 80.869° E | 21.161° | 2025-12-07 07:39:38.332Z | 28.672° NE |
| 10 mins | 2025-12-07 09:16:38.332Z | 201.306° SSW | 2025-12-07 09:20:38.332Z | 256.877° W | 39.21° | 2025-12-07 09:26:38.332Z | 348.062° N |
| 11 mins | 2025-12-07 20:25:38.332Z | 7.245° NNE | 2025-12-07 20:30:38.332Z | 86.516° E | 43.668° | 2025-12-07 20:36:38.332Z | 173.62° S |
| 6 mins | 2025-12-07 22:13:38.332Z | 315.907° NNW | 2025-12-07 22:16:38.332Z | 285.095° WNW | 17.008° | 2025-12-07 22:19:38.332Z | 255.304° W |
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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