GESAT GEN 1, 62612
Orbit data source: Space-Track
GESAT GEN 1, 62612 is a French payload satellite in SSO that was launched on Tue, 14 Jan 2025 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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62612 intel report (Beta)
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Identifier
Orbit
Country
FRRelated business
Manufacturer
NanoAvionics
Mission
Operational Commercial Earth Obs Sci
Bus & Motor
CUBESAT 16U MP42, Unknown motor
Mass
30 kg wet, 30 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.146 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 GESAT GEN 1
1 62612U 25009D 26215.79668209 .00008435 00000-0 29903-3 0 9992
2 62612 97.3997 297.5872 0002271 105.3143 254.8348 15.29336896 86192Epoch: 2026-08-03T19:07Z
TLE epoch observation values (Epoch: 2026-08-03T19:07:13.332Z)
Latitude
-0.00006°
Longitude
58.40701°
Altitude
481.304 km
Speed
7.625 km/s
True Right ascension
19h 50m 20s
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
20:02:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.303 km
Perigee altitude
473.19 km
Semi-major axis
6,852.883 km
Eccentricity
0.00023
Inclination
97.3997°
RAAN
297.5872°
Arg. of periapsis
105.3143°
True anomaly
254.80968°
Mean anomaly
254.8348°
Eccentric anomaly
254.82224°
Mean motion
3.8259 °/min
Orbital period
94.1 mins
BSTAR
0.00029903
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.GESAT GEN 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-05 18:47:48.152Z | 348.275° N | 2026-08-05 18:49:48.152Z | 295.209° NW | 32.864° | 2026-08-05 18:52:48.152Z | 218.644° SW |
| 5 mins | 2026-08-06 05:21:48.152Z | 149.363° SSE | 2026-08-06 05:23:48.152Z | 88.998° E | 40.379° | 2026-08-06 05:26:48.152Z | 358.011° 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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