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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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, 5.0 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 26305.81453547 .00000096 00000-0 13015-3 0 9991
2 62800 88.9726 69.4400 0016643 117.7935 242.4906 13.50909301 90999Epoch: 2026-11-01T19:32Z
TLE epoch observation values (Epoch: 2026-11-01T19:32:55.864Z)
Latitude
0.00001°
Longitude
95.10673°
Altitude
1,077.61 km
Speed
7.31 km/s
True Right ascension
04h 37m 45s
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
22:56:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.355 km
Perigee altitude
1,053.577 km
Semi-major axis
7,444.103 km
Eccentricity
0.00166
Inclination
88.9726°
RAAN
69.44°
Arg. of periapsis
117.7935°
True anomaly
242.32161°
Mean anomaly
242.4906°
Eccentric anomaly
242.40609°
Mean motion
3.37928 °/min
Orbital period
106.53 mins
BSTAR
0.00013015
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-11-02 08:06:16.020Z | 146.212° SSE | 2026-11-02 08:11:16.020Z | 87.588° E | 42.387° | 2026-11-02 08:17:16.020Z | 14.432° NNE |
| 9 mins | 2026-11-02 09:54:16.020Z | 229.894° WSW | 2026-11-02 09:58:16.020Z | 279.831° WNW | 30.054° | 2026-11-02 10:03:16.020Z | 334.86° NNW |
| 7 mins | 2026-11-02 19:17:16.020Z | 43.291° NE | 2026-11-02 19:20:16.020Z | 75.421° E | 20.188° | 2026-11-02 19:24:16.020Z | 117.287° SE |
| 11 mins | 2026-11-02 21:02:16.020Z | 351.626° N | 2026-11-02 21:07:16.020Z | 285.387° WNW | 62.195° | 2026-11-02 21:13:16.020Z | 197.735° 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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