Showing default

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.

Loading next visibility...
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 (11 months 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: 14 hours ago

TLE from 14 hours ago
0 GESAT GEN 1
1 62612U 25009D   25354.18521237  .00006203  00000-0  25093-3 0  9994
2 62612  97.4192  72.5842 0001343 118.2442 241.8932 15.25072413 51603
Epoch: 2025-12-20T04:26Z
TLE epoch observation values (Epoch: 2025-12-20T04:26:42.348Z)
Latitude
0.00001°
Longitude
-83.10789°
Altitude
494.1 km
Speed
7.617 km/s
True Right ascension
04h 50m 20s
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
17:40:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
488.45 km
Perigee altitude
486.606 km
Semi-major axis
6,865.665 km
Eccentricity
0.00013
Inclination
97.4192°
RAAN
72.5842°
Arg. of periapsis
118.2442°
True anomaly
241.87963°
Mean anomaly
241.8932°
Eccentric anomaly
241.88641°
Mean motion
3.81522 °/min
Orbital period
94.36 mins
BSTAR
0.00025093
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|