LEONAV-1, 69937
Orbit data source: Space-Track
LEONAV-1, 69937 is a French payload satellite in SSO that was launched on Tue, 07 Jul 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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69937 intel report (Beta)
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Identifier
Orbit
Country
FRRelated business
Manufacturer
U-Space
Mission
Operational spacecraft
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
~15 kg wet, ~15 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
BOX+ 2 PAN, 1.0 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 LEONAV-1
1 69937U 26156BW 26236.47041404 .00002775 00000-0 27311-3 0 9995
2 69937 97.7462 136.1881 0010926 3.3648 356.7643 14.92855245 7186Epoch: 2026-08-24T11:17Z
TLE epoch observation values (Epoch: 2026-08-24T11:17:23.773Z)
Latitude
0.00001°
Longitude
-5.91261°
Altitude
584.48 km
Speed
7.572 km/s
True Right ascension
09h 04m 45s
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
02:01:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
593.664 km
Perigee altitude
578.446 km
Semi-major axis
6,964.192 km
Eccentricity
0.00109
Inclination
97.7462°
RAAN
136.1881°
Arg. of periapsis
3.3648°
True anomaly
356.75722°
Mean anomaly
356.7643°
Eccentric anomaly
356.76076°
Mean motion
3.73454 °/min
Orbital period
96.4 mins
BSTAR
0.00027311
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Other satellites on launch #156 in the year 2026 (2026-07-07 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.LEONAV-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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-25 16:24:35.560Z | 99.087° ESE | 2026-08-25 16:26:35.560Z | 64.736° ENE | 17.143° | 2026-08-25 16:28:35.560Z | 31.716° NE |
| 5 mins | 2026-08-25 17:59:35.560Z | 210.514° SW | 2026-08-25 18:01:35.560Z | 258.37° W | 29.741° | 2026-08-25 18:04:35.560Z | 322.597° NNW |
| 5 mins | 2026-08-26 05:42:35.560Z | 49.003° ENE | 2026-08-26 05:44:35.560Z | 97.278° ESE | 28.925° | 2026-08-26 05:47:35.560Z | 157.018° SSE |
| 4 mins | 2026-08-26 07:18:35.560Z | 316.072° NNW | 2026-08-26 07:19:35.560Z | 297.762° NW | 18.185° | 2026-08-26 07:22:35.560Z | 249.365° W |
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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