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, 1.3 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 QIANFAN-68
1 62798U 25016P 25306.46421851 .00000065 00000-0 81691-4 0 9993
2 62798 88.9743 107.2594 0016750 99.8999 260.4044 13.50973352 41804Epoch: 2025-11-02T11:08Z
TLE epoch observation values (Epoch: 2025-11-02T11:08:28.479Z)
Latitude
0.00001°
Longitude
-101.83883°
Altitude
1,073.733 km
Speed
7.314 km/s
True Right ascension
07h 09m 02s
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
14:41:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.199 km
Perigee altitude
1,053.262 km
Semi-major axis
7,443.868 km
Eccentricity
0.00168
Inclination
88.9743°
RAAN
107.2594°
Arg. of periapsis
99.8999°
True anomaly
260.21521°
Mean anomaly
260.4044°
Eccentric anomaly
260.3098°
Mean motion
3.37944 °/min
Orbital period
106.53 mins
BSTAR
0.000081691
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-03 21:31:51.502Z | 39.442° NE | 2025-11-03 21:35:51.502Z | 77.992° E | 15.859° | 2025-11-03 21:38:51.502Z | 107.49° ESE |
| 11 mins | 2025-11-03 23:17:51.502Z | 355.777° N | 2025-11-03 23:22:51.502Z | 275.26° WNW | 44.015° | 2025-11-03 23:28:51.502Z | 190.4° SSW |
| 4 mins | 2025-11-04 09:32:51.502Z | 85.361° E | 2025-11-04 09:33:51.502Z | 75.464° E | 13.939° | 2025-11-04 09:36:51.502Z | 46.479° ENE |
| 11 mins | 2025-11-04 11:14:51.502Z | 180.216° SSW | 2025-11-04 11:19:51.502Z | 260.079° W | 44.894° | 2025-11-04 11:25:51.502Z | 357.865° N |
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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