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: 6 hours ago
TLE from 6 hours ago
0 QIANFAN-72
1 62802U 25016T 26305.82518833 .00000104 00000-0 14142-3 0 9996
2 62802 88.9710 69.3803 0020413 136.7763 223.4994 13.51033230 90985Epoch: 2026-11-01T19:48Z
TLE epoch observation values (Epoch: 2026-11-01T19:48:16.271Z)
Latitude
-0.00009°
Longitude
91.2015°
Altitude
1,082.456 km
Speed
7.305 km/s
True Right ascension
04h 37m 31s
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
21:42:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,080.705 km
Perigee altitude
1,050.316 km
Semi-major axis
7,443.648 km
Eccentricity
0.00204
Inclination
88.971°
RAAN
69.3803°
Arg. of periapsis
136.7763°
True anomaly
223.33868°
Mean anomaly
223.4994°
Eccentric anomaly
223.41901°
Mean motion
3.37959 °/min
Orbital period
106.52 mins
BSTAR
0.00014142
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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 | 2026-11-02 08:20:23.611Z | 159.282° S | 2026-11-02 08:26:23.611Z | 95.098° ESE | 55.623° | 2026-11-02 08:32:23.611Z | 9.637° NNE |
| 8 mins | 2026-11-02 10:10:23.611Z | 244.454° WSW | 2026-11-02 10:13:23.611Z | 278.218° WNW | 22.89° | 2026-11-02 10:18:23.611Z | 329.601° NNW |
| 8 mins | 2026-11-02 19:32:23.611Z | 38.101° NE | 2026-11-02 19:35:23.611Z | 73.549° E | 26.401° | 2026-11-02 19:40:23.611Z | 130.861° SE |
| 11 mins | 2026-11-02 21:17:23.611Z | 345.75° N | 2026-11-02 21:22:23.611Z | 283.545° WNW | 47.18° | 2026-11-02 21:28:23.611Z | 207.781° 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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