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: 11 hours ago
TLE from 11 hours ago
0 FLYLAB 2
1 68503U 26067CR 26255.25002315 .00081184 00000-0 75490-2 0 9990
2 68503 97.7673 211.9126 0007444 141.8122 110.1552 14.93917451 3106Epoch: 2026-09-12T06:00Z
TLE epoch observation values (Epoch: 2026-09-12T06:00:02.000Z)
Latitude
-70.63593°
Longitude
-72.06343°
Altitude
613.837 km
Speed
7.55 km/s
True Right ascension
00h 36m 49s
True Declination
-70° 31' 33"
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
09:04:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.933 km
Perigee altitude
577.57 km
Semi-major axis
6,960.888 km
Eccentricity
0.00074
Inclination
97.7673°
RAAN
211.9126°
Arg. of periapsis
141.8122°
True anomaly
110.23525°
Mean anomaly
110.1552°
Eccentric anomaly
110.19523°
Mean motion
3.7372 °/min
Orbital period
96.33 mins
BSTAR
0.007549
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-09-12 21:03:58.270Z | 158.565° S | 2026-09-12 21:07:58.270Z | 69.739° E | 70.388° | 2026-09-12 21:11:58.270Z | 352.531° N |
| 6 mins | 2026-09-13 10:22:58.270Z | 358.807° N | 2026-09-13 10:25:58.270Z | 270.784° WNW | 55.635° | 2026-09-13 10:28:58.270Z | 210.295° 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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