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: 6 hours ago
TLE from 6 hours ago
0 QIANFAN-68
1 62798U 25016P 26035.82199954 .00000124 00000-0 17387-3 0 9995
2 62798 88.9734 97.5135 0015484 180.2013 179.9134 13.50990141 54545Epoch: 2026-02-04T19:43Z
TLE epoch observation values (Epoch: 2026-02-04T19:43:40.760Z)
Latitude
-0.00007°
Longitude
26.61059°
Altitude
1,083.104 km
Speed
7.305 km/s
True Right ascension
06h 30m 03s
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
03:18:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.195 km
Perigee altitude
1,054.143 km
Semi-major axis
7,443.806 km
Eccentricity
0.00155
Inclination
88.9734°
RAAN
97.5135°
Arg. of periapsis
180.2013°
True anomaly
179.91367°
Mean anomaly
179.9134°
Eccentric anomaly
179.91353°
Mean motion
3.37949 °/min
Orbital period
106.53 mins
BSTAR
0.00017387
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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 | 2026-02-05 02:59:25.142Z | 108.667° ESE | 2026-02-05 03:03:25.142Z | 67.835° E | 17.78° | 2026-02-05 03:06:25.142Z | 38.293° NE |
| 11 mins | 2026-02-05 04:43:25.142Z | 189.549° SSW | 2026-02-05 04:48:25.142Z | 250.753° W | 42.797° | 2026-02-05 04:54:25.142Z | 352.687° N |
| 11 mins | 2026-02-05 15:53:25.142Z | 12.753° NNE | 2026-02-05 15:58:25.142Z | 90.924° ESE | 40.544° | 2026-02-05 16:04:25.142Z | 166.061° S |
| 7 mins | 2026-02-05 17:41:25.142Z | 317.951° NNW | 2026-02-05 17:44:25.142Z | 283.878° WNW | 20.288° | 2026-02-05 17:48:25.142Z | 242.659° 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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