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, 1.3 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-68
1 62798U 25016P 26141.88046084 .00000103 00000-0 14118-3 0 9990
2 62798 88.9727 86.4853 0012846 237.8854 122.1051 13.51011537 68864Epoch: 2026-05-21T21:07Z
TLE epoch observation values (Epoch: 2026-05-21T21:07:51.816Z)
Latitude
-0.00002°
Longitude
-109.99991°
Altitude
1,076.586 km
Speed
7.311 km/s
True Right ascension
05h 45m 56s
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
15:20:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.153 km
Perigee altitude
1,056.028 km
Semi-major axis
7,443.727 km
Eccentricity
0.00128
Inclination
88.9727°
RAAN
86.4853°
Arg. of periapsis
237.8854°
True anomaly
122.22969°
Mean anomaly
122.1051°
Eccentric anomaly
122.1674°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.00014118
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-05-22 08:23:32.557Z | 6.016° NNE | 2026-05-22 08:29:32.557Z | 105.962° ESE | 43.514° | 2026-05-22 08:35:32.557Z | 173.88° S |
| 6 mins | 2026-05-22 10:12:32.557Z | 313.605° NW | 2026-05-22 10:15:32.557Z | 282.116° WNW | 16.833° | 2026-05-22 10:18:32.557Z | 253.051° W |
| 11 mins | 2026-05-22 20:21:32.557Z | 159.801° S | 2026-05-22 20:26:32.557Z | 69.446° E | 41.563° | 2026-05-22 20:32:32.557Z | 6.153° NNE |
| 8 mins | 2026-05-22 22:09:32.557Z | 243.904° WSW | 2026-05-22 22:13:32.557Z | 285.974° WNW | 19.169° | 2026-05-22 22:17:32.557Z | 325.274° NNW |
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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