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: 9 hours ago
TLE from 9 hours ago
0 FOSSASAT2E19 (TAT-E)
1 62676U 25009BV 26171.46382036 .00001948 00000-0 90499-4 0 9999
2 62676 97.3957 249.6829 0004342 345.0611 15.0496 15.21163504 79191Epoch: 2026-06-20T11:07Z
TLE epoch observation values (Epoch: 2026-06-20T11:07:54.079Z)
Latitude
0.00002°
Longitude
174.02949°
Altitude
502.537 km
Speed
7.615 km/s
True Right ascension
16h 38m 43s
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
07:21:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.28 km
Perigee altitude
496.308 km
Semi-major axis
6,877.431 km
Eccentricity
0.00043
Inclination
97.3957°
RAAN
249.6829°
Arg. of periapsis
345.0611°
True anomaly
15.06253°
Mean anomaly
15.0496°
Eccentric anomaly
15.05606°
Mean motion
3.80543 °/min
Orbital period
94.6 mins
BSTAR
0.000090499
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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 | 2026-06-21 04:38:31.894Z | 123.657° SE | 2026-06-21 04:40:31.894Z | 84.339° E | 24.088° | 2026-06-21 04:43:31.894Z | 17.526° NNE |
| 5 mins | 2026-06-21 17:42:31.894Z | 38.546° NE | 2026-06-21 17:44:31.894Z | 94.384° ESE | 32.982° | 2026-06-21 17:47:31.894Z | 166.374° S |
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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