Showing default

FOSSASAT2E22, 66779

Orbit data source: Space-Track

FOSSASAT2E22, 66779 is a Spanish payload satellite in SSO that was launched on Fri, 28 Nov 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
66779, 2025-276DU
Orbit
SSO
Country
Flag of ESES / SPN
Related business
Manufacturer
Fossa Systems
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
2025-11-28 (4 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, 0.1 m
Radar Cross Section
0.035 m²

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 FOSSASAT2E22
1 66779U 25276DU  26091.93586013  .00013088  00000-0  64646-3 0  9999
2 66779  97.4231 166.6027 0006502  54.8970 305.2873 15.17976559 18830
Epoch: 2026-04-01T22:27Z
TLE epoch observation values (Epoch: 2026-04-01T22:27:38.315Z)
Latitude
0.00002°
Longitude
-0.5985°
Altitude
512.457 km
Speed
7.609 km/s
True Right ascension
11h 06m 24s
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
04:49:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.404 km
Perigee altitude
504.448 km
Semi-major axis
6,887.063 km
Eccentricity
0.00065
Inclination
97.4231°
RAAN
166.6027°
Arg. of periapsis
54.897°
True anomaly
305.22645°
Mean anomaly
305.2873°
Eccentric anomaly
305.25688°
Mean motion
3.79745 °/min
Orbital period
94.8 mins
BSTAR
0.00064646
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
|