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FOSSASAT2E20 (TAT-O), 63003

Orbit data source: Space-Track

FOSSASAT2E20 (TAT-O), 63003 is a payload satellite owned by Fossa Systems (ES) 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
63003, 2025-009DN
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)
2025-01-14 (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, 0.4 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 FOSSASAT2E20 (TAT-O)
1 63003U 25009DN  25335.17073544  .00016136  00000-0  67803-3 0  9991
2 63003  97.3402  49.7301 0002450 330.1532  29.9565 15.23506524106298
Epoch: 2025-12-01T04:05Z
TLE epoch observation values (Epoch: 2025-12-01T04:05:51.542Z)
Latitude
-0.00001°
Longitude
-82.00873°
Altitude
496.911 km
Speed
7.617 km/s
True Right ascension
03h 18m 55s
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
12:50:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.915 km
Perigee altitude
490.549 km
Semi-major axis
6,870.369 km
Eccentricity
0.00025
Inclination
97.3402°
RAAN
49.7301°
Arg. of periapsis
330.1532°
True anomaly
29.97052°
Mean anomaly
29.9565°
Eccentric anomaly
29.96351°
Mean motion
3.8113 °/min
Orbital period
94.46 mins
BSTAR
0.00067803
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