QIANFAN-242, 100695
Orbit data source: Space-Track
QIANFAN-242, 100695 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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100695 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
Mission
Operational spacecraft
Bus & Motor
QIANFAN, Unknown motor
Mass
267 kg wet, ~267 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
BOX+PAN, 5.0 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 QIANFAN-242
1 A0695U 26210D 26260.89261642 .00000053 00000-0 28253-4 0 9997
2 A0695 89.0031 12.6491 0007439 285.5011 74.5344 13.97458007 372Epoch: 2026-09-17T21:25Z
TLE epoch observation values (Epoch: 2026-09-17T21:25:22.058Z)
Latitude
-0.00011°
Longitude
54.48386°
Altitude
904.191 km
Speed
7.401 km/s
True Right ascension
00h 50m 35s
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
02:29:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
905.008 km
Perigee altitude
894.181 km
Semi-major axis
7,277.732 km
Eccentricity
0.00074
Inclination
89.0031°
RAAN
12.6491°
Arg. of periapsis
285.5011°
True anomaly
74.61658°
Mean anomaly
74.5344°
Eccentric anomaly
74.57549°
Mean motion
3.49582 °/min
Orbital period
102.98 mins
BSTAR
0.000028253
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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-242 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 09:40:42.821Z | 265.093° W | 2026-09-19 09:42:42.821Z | 285.489° WNW | 11.78° | 2026-09-19 09:44:42.821Z | 305.814° NW |
| 8 mins | 2026-09-19 18:42:42.821Z | 36.97° NE | 2026-09-19 18:45:42.821Z | 74.815° E | 24.699° | 2026-09-19 18:50:42.821Z | 134.393° SE |
| 9 mins | 2026-09-19 20:25:42.821Z | 337.763° N | 2026-09-19 20:29:42.821Z | 265.611° W | 42.417° | 2026-09-19 20:34:42.821Z | 208.497° SW |
| 4 mins | 2026-09-20 06:18:42.821Z | 88.537° E | 2026-09-20 06:20:42.821Z | 66.837° ENE | 13.14° | 2026-09-20 06:22:42.821Z | 46.455° ENE |
| 10 mins | 2026-09-20 07:57:42.821Z | 182.349° SSW | 2026-09-20 08:02:42.821Z | 310.262° NW | 77.866° | 2026-09-20 08:07:42.821Z | 356.589° 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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