Showing default

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.

Loading next visibility...
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 (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, 0.4 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 FOSSASAT2E20 (TAT-O)
1 63003U 25009DN  26126.14574209  .00014088  00000-0  50723-3 0  9998
2 63003  97.3172 202.7015 0004520 116.3293 243.8412 15.28681273130085
Epoch: 2026-05-06T03:29Z
TLE epoch observation values (Epoch: 2026-05-06T03:29:52.116Z)
Latitude
-0°
Longitude
-73.77608°
Altitude
484.226 km
Speed
7.622 km/s
True Right ascension
13h 30m 48s
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
20:28:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
479.802 km
Perigee altitude
473.606 km
Semi-major axis
6,854.841 km
Eccentricity
0.00045
Inclination
97.3172°
RAAN
202.7015°
Arg. of periapsis
116.3293°
True anomaly
243.79472°
Mean anomaly
243.8412°
Eccentric anomaly
243.81796°
Mean motion
3.82426 °/min
Orbital period
94.14 mins
BSTAR
0.00050723
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
|