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 spacecraft
Bus & Motor
CUBESAT 8U, Unknown motor
Mass
15 kg wet, ~15 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 FLYLAB 1
1 68472U 26067BJ 26171.38477755 .00001753 00000-0 18322-3 0 9996
2 68472 97.7630 129.5052 0005374 45.7184 314.4475 14.90920394 12207Epoch: 2026-06-20T09:14Z
TLE epoch observation values (Epoch: 2026-06-20T09:14:04.780Z)
Latitude
0.00005°
Longitude
82.38511°
Altitude
595.481 km
Speed
7.564 km/s
True Right ascension
08h 38m 01s
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
07:13:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
595.83 km
Perigee altitude
588.339 km
Semi-major axis
6,970.222 km
Eccentricity
0.00054
Inclination
97.763°
RAAN
129.5052°
Arg. of periapsis
45.7184°
True anomaly
314.40352°
Mean anomaly
314.4475°
Eccentric anomaly
314.42551°
Mean motion
3.72969 °/min
Orbital period
96.52 mins
BSTAR
0.00018322
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-20 20:38:46.147Z | 131.385° SE | 2026-06-20 20:41:46.147Z | 75.012° E | 28.928° | 2026-06-20 20:44:46.147Z | 13.029° NNE |
| 4 mins | 2026-06-20 22:15:46.147Z | 235.088° WSW | 2026-06-20 22:17:46.147Z | 270.007° WNW | 17.389° | 2026-06-20 22:19:46.147Z | 302.8° NW |
| 6 mins | 2026-06-21 09:58:46.147Z | 21.32° NNE | 2026-06-21 10:00:46.147Z | 53.694° ENE | 41.571° | 2026-06-21 10:04:46.147Z | 184.899° SSW |
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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