FLYLAB 2, 68503
Orbit data source: Space-Track
FLYLAB 2, 68503 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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68503 intel report (Beta)
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Identifier
Orbit
Country
FRRelated business
Manufacturer
NanoAvionics
Mission
Operational Civil Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan, 1.0 m
Radar Cross Section
0.139 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 FLYLAB 2
1 68503U 26067CR 26235.35097746 .00001611 00000-0 16808-3 0 9997
2 68503 97.7626 192.3215 0004945 180.4249 179.6966 14.91122046 21720Epoch: 2026-08-23T08:25Z
TLE epoch observation values (Epoch: 2026-08-23T08:25:24.452Z)
Latitude
-0.00003°
Longitude
94.32134°
Altitude
600.925 km
Speed
7.557 km/s
True Right ascension
12h 49m 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
18:16:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.902 km
Perigee altitude
588.009 km
Semi-major axis
6,969.593 km
Eccentricity
0.00049
Inclination
97.7626°
RAAN
192.3215°
Arg. of periapsis
180.4249°
True anomaly
179.6969°
Mean anomaly
179.6966°
Eccentric anomaly
179.69675°
Mean motion
3.7302 °/min
Orbital period
96.51 mins
BSTAR
0.00016808
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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 2 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 | 2026-08-24 09:10:40.750Z | 57.562° ENE | 2026-08-24 09:12:40.750Z | 92.325° ESE | 18.689° | 2026-08-24 09:15:40.750Z | 140.34° SSE |
| 5 mins | 2026-08-24 10:46:40.750Z | 331.054° NNW | 2026-08-24 10:48:40.750Z | 281.235° WNW | 27.159° | 2026-08-24 10:51:40.750Z | 229.866° WSW |
| 6 mins | 2026-08-24 21:35:40.750Z | 190.705° SSW | 2026-08-24 21:38:40.750Z | 268.964° W | 37.085° | 2026-08-24 21:41:40.750Z | 332.194° NNW |
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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