QIANFAN-68, 62798
Orbit data source: Space-Track
QIANFAN-68, 62798 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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62798 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, 5.0 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-68
1 62798U 25016P 25256.92359239 .00000033 00000-0 32380-4 0 9994
2 62798 88.9773 112.3856 0013477 242.0103 117.9686 13.52427869 35111Epoch: 2025-09-13T22:09Z
TLE epoch observation values (Epoch: 2025-09-13T22:09:58.382Z)
Latitude
0.00001°
Longitude
146.74236°
Altitude
1,071.009 km
Speed
7.314 km/s
True Right ascension
07h 29m 32s
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
00:20:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,070.413 km
Perigee altitude
1,050.363 km
Semi-major axis
7,438.525 km
Eccentricity
0.00135
Inclination
88.9773°
RAAN
112.3856°
Arg. of periapsis
242.0103°
True anomaly
118.10489°
Mean anomaly
117.9686°
Eccentric anomaly
118.03676°
Mean motion
3.38308 °/min
Orbital period
106.41 mins
BSTAR
0.00003238
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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-68 Visibility forecast
Loading observer location...
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 | 2025-09-14 14:15:01.543Z | 152.105° SSE | 2025-09-14 14:21:01.543Z | 76.173° E | 36.433° | 2025-09-14 14:27:01.543Z | 11.063° NNE |
| 9 mins | 2025-09-14 16:03:01.543Z | 230.035° WSW | 2025-09-14 16:07:01.543Z | 273.576° WNW | 24.305° | 2025-09-14 16:12:01.543Z | 330.265° NNW |
| 8 mins | 2025-09-15 01:26:01.543Z | 42.846° NE | 2025-09-15 01:29:01.543Z | 76.732° E | 20.933° | 2025-09-15 01:34:01.543Z | 127.504° SE |
| 11 mins | 2025-09-15 03:11:01.543Z | 348.618° N | 2025-09-15 03:16:01.543Z | 274.784° WNW | 39.89° | 2025-09-15 03:22:01.543Z | 200.853° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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