QIANFAN-240, 100693
Orbit data source: Space-Track
QIANFAN-240, 100693 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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100693 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
RCS unknown
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 QIANFAN-240
1 A0693U 26210B 26261.89509570 -.00002778 00000-0 -19888-2 0 9991
2 A0693 89.0041 12.5423 0007392 281.6749 78.3598 13.97438324 517Epoch: 2026-09-18T21:28Z
TLE epoch observation values (Epoch: 2026-09-18T21:28:56.268Z)
Latitude
-0.00009°
Longitude
52.49642°
Altitude
904.618 km
Speed
7.4 km/s
True Right ascension
00h 50m 10s
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
02:28:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
905.043 km
Perigee altitude
894.283 km
Semi-major axis
7,277.8 km
Eccentricity
0.00074
Inclination
89.0041°
RAAN
12.5423°
Arg. of periapsis
281.6749°
True anomaly
78.44278°
Mean anomaly
78.3598°
Eccentric anomaly
78.40129°
Mean motion
3.49577 °/min
Orbital period
102.98 mins
BSTAR
-0.0019888
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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-240 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 | 2026-09-19 18:43:12.664Z | 40.908° NE | 2026-09-19 18:46:12.664Z | 81.565° E | 24.899° | 2026-09-19 18:50:12.664Z | 130.413° SE |
| 9 mins | 2026-09-19 20:25:12.664Z | 341.303° N | 2026-09-19 20:29:12.664Z | 281.542° WNW | 43.063° | 2026-09-19 20:34:12.664Z | 210.767° SW |
| 10 mins | 2026-09-20 07:58:12.664Z | 182.861° SSW | 2026-09-20 08:02:12.664Z | 227.156° WSW | 77.551° | 2026-09-20 08:08:12.664Z | 356.906° 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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