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: 1 day ago
TLE from 1 day ago
0 FLYLAB 1
1 68472U 26067BJ 26307.60564078 .00001164 00000-0 11749-3 0 9999
2 68472 97.7825 263.8233 0002284 320.6322 39.4731 14.92989289 32517Epoch: 2026-11-03T14:32Z
TLE epoch observation values (Epoch: 2026-11-03T14:32:07.363Z)
Latitude
-0.00002°
Longitude
2.92672°
Altitude
590.435 km
Speed
7.566 km/s
True Right ascension
17h 35m 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
12:23:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.23 km
Perigee altitude
584.049 km
Semi-major axis
6,963.776 km
Eccentricity
0.00023
Inclination
97.7825°
RAAN
263.8233°
Arg. of periapsis
320.6322°
True anomaly
39.48974°
Mean anomaly
39.4731°
Eccentric anomaly
39.48142°
Mean motion
3.73487 °/min
Orbital period
96.39 mins
BSTAR
0.00011749
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-11-04 21:12:29.150Z | 165.041° S | 2026-11-04 21:16:29.150Z | 131.487° SE | 83.858° | 2026-11-04 21:20:29.150Z | 348.567° N |
| 6 mins | 2026-11-05 10:32:29.150Z | 350.893° N | 2026-11-05 10:35:29.150Z | 265.47° W | 43.375° | 2026-11-05 10:38:29.150Z | 216.468° SW |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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