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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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-72
1 62802U 25016T 26257.61098351 .00000036 00000-0 37826-4 0 9996
2 62802 88.9649 74.4061 0017157 279.8951 80.0263 13.51020526 84475Epoch: 2026-09-14T14:39Z
TLE epoch observation values (Epoch: 2026-09-14T14:39:48.975Z)
Latitude
-0.00004°
Longitude
-139.13676°
Altitude
1,069.267 km
Speed
7.318 km/s
True Right ascension
04h 57m 37s
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
15:36:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.328 km
Perigee altitude
1,052.786 km
Semi-major axis
7,443.694 km
Eccentricity
0.00172
Inclination
88.9649°
RAAN
74.4061°
Arg. of periapsis
279.8951°
True anomaly
80.22001°
Mean anomaly
80.0263°
Eccentric anomaly
80.12315°
Mean motion
3.37956 °/min
Orbital period
106.52 mins
BSTAR
0.000037826
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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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2026-09-15 00:07:58.641Z | 1.88° NNE | 2026-09-15 00:14:58.641Z | 146.914° SSE | 80.929° | 2026-09-15 00:20:58.641Z | 180.244° SSW |
| 5 mins | 2026-09-15 01:57:58.641Z | 310.806° NW | 2026-09-15 01:59:58.641Z | 291.603° WNW | 14.921° | 2026-09-15 02:02:58.641Z | 262.964° W |
| 12 mins | 2026-09-15 12:05:58.641Z | 168.596° S | 2026-09-15 12:10:58.641Z | 119.501° SE | 71.669° | 2026-09-15 12:17:58.641Z | 2.981° NNE |
| 6 mins | 2026-09-15 13:55:58.641Z | 257.125° W | 2026-09-15 13:58:58.641Z | 287.856° WNW | 17.044° | 2026-09-15 14:01:58.641Z | 316.904° NNW |
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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