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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62676 intel report (Beta)
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Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
Fossa Systems
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 FOSSASAT2E19 (TAT-E)
1 62676U 25009BV 26306.15675574 .00001747 00000-0 80022-4 0 9995
2 62676 97.3857 21.9415 0004468 197.8728 162.2352 15.21796861 99672Epoch: 2026-11-02T03:45Z
TLE epoch observation values (Epoch: 2026-11-02T03:45:43.695Z)
Latitude
-0.00002°
Longitude
-75.92837°
Altitude
506.442 km
Speed
7.609 km/s
True Right ascension
01h 27m 45s
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
10:35:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.455 km
Perigee altitude
494.311 km
Semi-major axis
6,875.52 km
Eccentricity
0.00045
Inclination
97.3857°
RAAN
21.9415°
Arg. of periapsis
197.8728°
True anomaly
162.25081°
Mean anomaly
162.2352°
Eccentric anomaly
162.24301°
Mean motion
3.80702 °/min
Orbital period
94.56 mins
BSTAR
0.000080022
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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.FOSSASAT2E19 (TAT-E) 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-02 18:32:32.875Z | 339.636° N | 2026-11-02 18:34:32.875Z | 276.106° WNW | 37.484° | 2026-11-02 18:37:32.875Z | 219.049° SW |
| 5 mins | 2026-11-03 05:09:32.875Z | 156.281° SSE | 2026-11-03 05:11:32.875Z | 41.425° NE | 70.712° | 2026-11-03 05:14:32.875Z | 352.578° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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