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
RCS unknown
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 FLYLAB 2
1 68503U 26067CR 26127.15836953 .00002130 00000-0 22326-3 0 9995
2 68503 97.7549 85.9814 0004926 178.7831 181.3400 14.90601231 5601Epoch: 2026-05-07T03:48Z
TLE epoch observation values (Epoch: 2026-05-07T03:48:03.127Z)
Latitude
-0.00002°
Longitude
163.95985°
Altitude
602.535 km
Speed
7.556 km/s
True Right ascension
05h 43m 55s
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
20:04:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
596.514 km
Perigee altitude
589.646 km
Semi-major axis
6,971.217 km
Eccentricity
0.00049
Inclination
97.7549°
RAAN
85.9814°
Arg. of periapsis
178.7831°
True anomaly
181.33868°
Mean anomaly
181.34°
Eccentric anomaly
181.33934°
Mean motion
3.7289 °/min
Orbital period
96.54 mins
BSTAR
0.00022326
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-07 20:04:29.095Z | 97.869° ESE | 2026-05-07 20:06:29.095Z | 68.846° E | 14.143° | 2026-05-07 20:08:29.095Z | 38.036° NE |
| 6 mins | 2026-05-07 21:39:29.095Z | 196.173° SSW | 2026-05-07 21:41:29.095Z | 239.731° WSW | 35.001° | 2026-05-07 21:45:29.095Z | 332.927° NNW |
| 5 mins | 2026-05-08 09:23:29.095Z | 48.867° ENE | 2026-05-08 09:25:29.095Z | 86.275° E | 23.866° | 2026-05-08 09:28:29.095Z | 145.821° SSE |
| 5 mins | 2026-05-08 10:59:29.095Z | 328.484° NNW | 2026-05-08 11:01:29.095Z | 288.95° WNW | 21.744° | 2026-05-08 11:04:29.095Z | 240.085° WSW |
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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