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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Edit Public Description
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: 17 hours ago
TLE from 17 hours ago
0 GESAT GEN 1
1 62612U 25009D 25308.69985405 .00009063 00000-0 37764-3 0 9995
2 62612 97.4236 27.5352 0001537 73.3558 286.7848 15.23938252 44675Epoch: 2025-11-04T16:47Z
TLE epoch observation values (Epoch: 2025-11-04T16:47:47.389Z)
Latitude
-0.00004°
Longitude
91.40463°
Altitude
496.766 km
Speed
7.616 km/s
True Right ascension
01h 50m 08s
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
05:49:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
491.993 km
Perigee altitude
489.881 km
Semi-major axis
6,869.074 km
Eccentricity
0.00015
Inclination
97.4236°
RAAN
27.5352°
Arg. of periapsis
73.3558°
True anomaly
286.76794°
Mean anomaly
286.7848°
Eccentric anomaly
286.77637°
Mean motion
3.81238 °/min
Orbital period
94.43 mins
BSTAR
0.00037764
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-05 18:34:10.661Z | 357.922° N | 2025-11-05 18:37:10.661Z | 276.96° WNW | 37.162° | 2025-11-05 18:40:10.661Z | 211.479° SW |
| 5 mins | 2025-11-06 05:11:10.661Z | 144.217° SSE | 2025-11-06 05:13:10.661Z | 78.414° E | 38.88° | 2025-11-06 05:16:10.661Z | 359.886° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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