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 spacecraft
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, ~10 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: 2 days ago
TLE from 2 days ago
0 FLYLAB 2
1 68503U 26067CR 26171.39372561 .00001460 00000-0 15417-3 0 9998
2 68503 97.7570 129.4360 0006767 60.2882 299.9009 14.90767971 12198Epoch: 2026-06-20T09:26Z
TLE epoch observation values (Epoch: 2026-06-20T09:26:57.892Z)
Latitude
-0.00003°
Longitude
79.0858°
Altitude
596.229 km
Speed
7.563 km/s
True Right ascension
08h 37m 44s
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
20:10:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
597.277 km
Perigee altitude
587.843 km
Semi-major axis
6,970.697 km
Eccentricity
0.00068
Inclination
97.757°
RAAN
129.436°
Arg. of periapsis
60.2882°
True anomaly
299.83365°
Mean anomaly
299.9009°
Eccentric anomaly
299.86728°
Mean motion
3.72931 °/min
Orbital period
96.53 mins
BSTAR
0.00015417
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-22 10:20:06.732Z | 4.159° NNE | 2026-06-22 10:24:06.732Z | 263.079° W | 40.764° | 2026-06-22 10:27:06.732Z | 207.517° SW |
| 7 mins | 2026-06-22 21:11:06.732Z | 162.411° S | 2026-06-22 21:14:06.732Z | 43.092° NE | 44.594° | 2026-06-22 21:18:06.732Z | 349.626° 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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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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