QIANFAN-246, 100699
Orbit data source: Space-Track
QIANFAN-246, 100699 is a Chinese payload satellite in LEO that was launched on Tue, 15 Sep 2026 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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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100699 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 QIANFAN-246
1 A0699U 26210H 26261.60855825 .00000045 00000-0 22767-4 0 9998
2 A0699 89.0040 12.5739 0007201 284.1438 75.8939 13.97493200 474Epoch: 2026-09-18T14:36Z
TLE epoch observation values (Epoch: 2026-09-18T14:36:19.432Z)
Latitude
-0.00005°
Longitude
155.96393°
Altitude
904.235 km
Speed
7.401 km/s
True Right ascension
00h 50m 17s
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
03:40:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
904.713 km
Perigee altitude
894.232 km
Semi-major axis
7,277.609 km
Eccentricity
0.00072
Inclination
89.004°
RAAN
12.5739°
Arg. of periapsis
284.1438°
True anomaly
75.97395°
Mean anomaly
75.8939°
Eccentric anomaly
75.93392°
Mean motion
3.49591 °/min
Orbital period
102.98 mins
BSTAR
0.000022767
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Other satellites on launch #210 in the year 2026 (2026-09-15 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-246 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-09-19 18:41:13.869Z | 27.155° NE | 2026-09-19 18:46:13.869Z | 85.776° E | 24.668° | 2026-09-19 18:50:13.869Z | 132.203° SE |
| 9 mins | 2026-09-19 20:25:13.869Z | 339.869° N | 2026-09-19 20:29:13.869Z | 274.031° WNW | 43.258° | 2026-09-19 20:34:13.869Z | 209.514° SW |
| 9 mins | 2026-09-20 07:58:13.869Z | 182.978° SSW | 2026-09-20 08:02:13.869Z | 268.51° W | 81.103° | 2026-09-20 08:07:13.869Z | 356.402° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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