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: 3 weeks ago
TLE from 3 weeks ago
0 QIANFAN-72
1 62802U 25016T 25274.29087208 .00000084 00000-0 11481-3 0 9998
2 62802 88.9730 110.6012 0018440 200.3911 159.6505 13.49486897 37447Epoch: 2025-10-01T06:58Z
TLE epoch observation values (Epoch: 2025-10-01T06:58:51.347Z)
Latitude
-0.00004°
Longitude
-4.38074°
Altitude
1,089.988 km
Speed
7.301 km/s
True Right ascension
07h 22m 24s
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
23:50:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,084.937 km
Perigee altitude
1,057.464 km
Semi-major axis
7,449.337 km
Eccentricity
0.00184
Inclination
88.973°
RAAN
110.6012°
Arg. of periapsis
200.3911°
True anomaly
159.72382°
Mean anomaly
159.6505°
Eccentric anomaly
159.68718°
Mean motion
3.37572 °/min
Orbital period
106.64 mins
BSTAR
0.00011481
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-22 10:19:42.034Z | 86.404° E | 2025-10-22 10:21:42.034Z | 68.179° E | 11.803° | 2025-10-22 10:23:42.034Z | 50.172° ENE |
| 12 mins | 2025-10-22 12:01:42.034Z | 173.078° S | 2025-10-22 12:06:42.034Z | 139.003° SSE | 44.352° | 2025-10-22 12:13:42.034Z | 1.061° NNE |
| 5 mins | 2025-10-22 13:52:42.034Z | 266.753° W | 2025-10-22 13:54:42.034Z | 286.659° WNW | 14.525° | 2025-10-22 13:57:42.034Z | 314.882° NW |
| 10 mins | 2025-10-22 23:12:42.034Z | 23° NE | 2025-10-22 23:17:42.034Z | 93.58° ESE | 32.557° | 2025-10-22 23:22:42.034Z | 149.979° SSE |
| 9 mins | 2025-10-23 00:59:42.034Z | 331.799° NNW | 2025-10-23 01:03:42.034Z | 282.157° WNW | 27.62° | 2025-10-23 01:08:42.034Z | 225.566° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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