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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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Identifier
62612, 2025-009D
Orbit
SSO
Country
Flag of FRFR
Related 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)
2025-01-14 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 GESAT GEN 1
1 62612U 25009D   26171.22884809  .00007217  00000-0  26176-3 0  9993
2 62612  97.4015 253.2561 0001061  93.4735 266.6626 15.28643546 79383
Epoch: 2026-06-20T05:29Z
TLE epoch observation values (Epoch: 2026-06-20T05:29:32.474Z)
Latitude
-0.00007°
Longitude
-97.57567°
Altitude
483.011 km
Speed
7.624 km/s
True Right ascension
16h 53m 01s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
11:43:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
477.548 km
Perigee altitude
476.093 km
Semi-major axis
6,854.957 km
Eccentricity
0.00011
Inclination
97.4015°
RAAN
253.2561°
Arg. of periapsis
93.4735°
True anomaly
266.65046°
Mean anomaly
266.6626°
Eccentric anomaly
266.65653°
Mean motion
3.82416 °/min
Orbital period
94.14 mins
BSTAR
0.00026176
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