QIANFAN-243, 100696
Orbit data source: Space-Track
QIANFAN-243, 100696 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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100696 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: 19 hours ago
TLE from 19 hours ago
0 QIANFAN-243
1 A0696U 26210E 26261.60860833 .00000045 00000-0 22631-4 0 9990
2 A0696 89.0049 12.5723 0007173 282.5061 77.5314 13.97472347 470Epoch: 2026-09-18T14:36Z
TLE epoch observation values (Epoch: 2026-09-18T14:36:23.759Z)
Latitude
-0.00002°
Longitude
155.94426°
Altitude
904.458 km
Speed
7.4 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
02:29:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
904.765 km
Perigee altitude
894.324 km
Semi-major axis
7,277.682 km
Eccentricity
0.00072
Inclination
89.0049°
RAAN
12.5723°
Arg. of periapsis
282.5061°
True anomaly
77.61167°
Mean anomaly
77.5314°
Eccentric anomaly
77.57154°
Mean motion
3.49586 °/min
Orbital period
102.98 mins
BSTAR
0.000022631
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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-243 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-19 09:40:35.628Z | 264.574° W | 2026-09-19 09:42:35.628Z | 284.925° WNW | 11.796° | 2026-09-19 09:44:35.628Z | 305.319° NW |
| 8 mins | 2026-09-19 18:42:35.628Z | 36.589° NE | 2026-09-19 18:45:35.628Z | 74.085° E | 24.609° | 2026-09-19 18:50:35.628Z | 134.049° SE |
| 9 mins | 2026-09-19 20:25:35.628Z | 338.124° N | 2026-09-19 20:29:35.628Z | 266.807° W | 42.627° | 2026-09-19 20:34:35.628Z | 208.605° SW |
| 4 mins | 2026-09-20 06:18:35.628Z | 88.941° E | 2026-09-20 06:20:35.628Z | 67.289° ENE | 13.134° | 2026-09-20 06:22:35.628Z | 46.841° ENE |
| 10 mins | 2026-09-20 07:57:35.628Z | 182.242° SSW | 2026-09-20 08:02:35.628Z | 306.483° NW | 78.634° | 2026-09-20 08:07:35.628Z | 356.584° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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