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: 12 hours ago
TLE from 12 hours ago
0 QIANFAN-72
1 62802U 25016T 26035.49686651 .00000121 00000-0 16916-3 0 9993
2 62802 88.9718 97.5392 0018935 194.3350 165.7266 13.50993403 54488Epoch: 2026-02-04T11:55Z
TLE epoch observation values (Epoch: 2026-02-04T11:55:29.266Z)
Latitude
-0.00006°
Longitude
144.00465°
Altitude
1,085.228 km
Speed
7.303 km/s
True Right ascension
06h 30m 09s
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
01:51:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,079.752 km
Perigee altitude
1,051.562 km
Semi-major axis
7,443.794 km
Eccentricity
0.00189
Inclination
88.9718°
RAAN
97.5392°
Arg. of periapsis
194.335°
True anomaly
165.77997°
Mean anomaly
165.7266°
Eccentric anomaly
165.7533°
Mean motion
3.37949 °/min
Orbital period
106.52 mins
BSTAR
0.00016916
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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 | 2026-02-05 04:00:50.356Z | 161.233° S | 2026-02-05 04:06:50.356Z | 101.497° ESE | 40.282° | 2026-02-05 04:12:50.356Z | 8.981° NNE |
| 8 mins | 2026-02-05 05:50:50.356Z | 244.353° WSW | 2026-02-05 05:53:50.356Z | 276.537° WNW | 20.41° | 2026-02-05 05:58:50.356Z | 327.852° NNW |
| 9 mins | 2026-02-05 15:12:50.356Z | 35.414° NE | 2026-02-05 15:16:50.356Z | 85.351° E | 25.136° | 2026-02-05 15:21:50.356Z | 137.129° SSE |
| 10 mins | 2026-02-05 16:58:50.356Z | 341.063° N | 2026-02-05 17:02:50.356Z | 288.414° WNW | 35.043° | 2026-02-05 17:08:50.356Z | 210.259° 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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