FLYLAB 1, 68472
Orbit data source: Space-Track
FLYLAB 1, 68472 is a payload satellite owned by ONERA (FR) in SSO that was launched on Mon, 30 Mar 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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68472 intel report (Beta)
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Identifier
Orbit
Country
FRRelated business
Manufacturer
NanoAvionics
Mission
Operational Civil Technology
Bus & Motor
CUBESAT 8U, Unknown motor
Mass
15 kg wet, ~15 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan, 1.0 m
Radar Cross Section
0.159 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 4 days ago
TLE from 4 days ago
0 FLYLAB 1
1 68472U 26067BJ 26259.54399867 .00000869 00000-0 91184-4 0 9993
2 68472 97.7731 216.3281 0005277 98.5027 261.6790 14.92051137 25346Epoch: 2026-09-16T13:03Z
TLE epoch observation values (Epoch: 2026-09-16T13:03:21.485Z)
Latitude
-0.00001°
Longitude
24.99451°
Altitude
595.117 km
Speed
7.562 km/s
True Right ascension
14h 25m 18s
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
05:12:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.236 km
Perigee altitude
584.884 km
Semi-major axis
6,966.697 km
Eccentricity
0.00053
Inclination
97.7731°
RAAN
216.3281°
Arg. of periapsis
98.5027°
True anomaly
261.61917°
Mean anomaly
261.679°
Eccentric anomaly
261.64909°
Mean motion
3.73253 °/min
Orbital period
96.45 mins
BSTAR
0.000091184
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Other satellites on launch #67 in the year 2026 (2026-03-30 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.FLYLAB 1 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-20 20:13:21.358Z | 103.978° ESE | 2026-09-20 20:15:21.358Z | 72.306° E | 18.007° | 2026-09-20 20:18:21.358Z | 24.937° NE |
| 6 mins | 2026-09-20 21:48:21.358Z | 204.844° SW | 2026-09-20 21:51:21.358Z | 276.888° WNW | 34.711° | 2026-09-20 21:54:21.358Z | 327.103° NNW |
| 5 mins | 2026-09-21 09:32:21.358Z | 51.417° ENE | 2026-09-21 09:34:21.358Z | 102.299° ESE | 33.336° | 2026-09-21 09:37:21.358Z | 158.375° S |
| 4 mins | 2026-09-21 11:08:21.358Z | 314.286° NW | 2026-09-21 11:09:21.358Z | 295.682° NW | 19.214° | 2026-09-21 11:12:21.358Z | 248.274° W |
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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