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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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-68
1 62798U 25016P 26305.77998535 .00000103 00000-0 14044-3 0 9995
2 62798 88.9726 69.4367 0016649 125.2825 234.9886 13.51034722 90995Epoch: 2026-11-01T18:43Z
TLE epoch observation values (Epoch: 2026-11-01T18:43:10.734Z)
Latitude
-0.00004°
Longitude
107.57552°
Altitude
1,078.536 km
Speed
7.309 km/s
True Right ascension
04h 37m 44s
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
22:57:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.898 km
Perigee altitude
1,053.112 km
Semi-major axis
7,443.642 km
Eccentricity
0.00166
Inclination
88.9726°
RAAN
69.4367°
Arg. of periapsis
125.2825°
True anomaly
234.83253°
Mean anomaly
234.9886°
Eccentric anomaly
234.91055°
Mean motion
3.3796 °/min
Orbital period
106.52 mins
BSTAR
0.00014044
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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
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-11-02 07:18:26.975Z | 110.365° ESE | 2026-11-02 07:22:26.975Z | 71.919° E | 17.699° | 2026-11-02 07:26:26.975Z | 34.138° NE |
| 11 mins | 2026-11-02 09:03:26.975Z | 188.549° SSW | 2026-11-02 09:08:26.975Z | 292.761° NW | 71.234° | 2026-11-02 09:14:26.975Z | 354.815° N |
| 11 mins | 2026-11-02 20:12:26.975Z | 13.021° NNE | 2026-11-02 20:17:26.975Z | 79.559° E | 55.443° | 2026-11-02 20:23:26.975Z | 163.285° S |
| 8 mins | 2026-11-02 22:00:26.975Z | 321.432° NNW | 2026-11-02 22:03:26.975Z | 287.825° WNW | 22.9° | 2026-11-02 22:08:26.975Z | 236.776° WSW |
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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