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FOSSASAT2E19 (TAT-E), 62676

Orbit data source: Space-Track

FOSSASAT2E19 (TAT-E), 62676 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
62676, 2025-009BV
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, 0.2 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 FOSSASAT2E19 (TAT-E)
1 62676U 25009BV  25335.15177148  .00003931  00000-0  18785-3 0  9993
2 62676  97.4152  51.9793 0004380 325.8790  34.2163 15.19595367 48608
Epoch: 2025-12-01T03:38Z
TLE epoch observation values (Epoch: 2025-12-01T03:38:33.055Z)
Latitude
-0.00003°
Longitude
-72.91381°
Altitude
507.658 km
Speed
7.612 km/s
True Right ascension
03h 27m 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
12:50:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.044 km
Perigee altitude
501.015 km
Semi-major axis
6,882.166 km
Eccentricity
0.00044
Inclination
97.4152°
RAAN
51.9793°
Arg. of periapsis
325.879°
True anomaly
34.24454°
Mean anomaly
34.2163°
Eccentric anomaly
34.23042°
Mean motion
3.8015 °/min
Orbital period
94.7 mins
BSTAR
0.00018785
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