FOSSASAT2E18 (TAT-A), 62686
Orbit data source: Space-Track
FOSSASAT2E18 (TAT-A), 62686 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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62686 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: 15 hours ago
TLE from 15 hours ago
0 FOSSASAT2E18 (TAT-A)
1 62686U 25009CF 26307.17540075 .00001715 00000-0 78957-4 0 9995
2 62686 97.3870 23.0036 0005404 194.5655 165.5426 15.21641898 99828Epoch: 2026-11-03T04:12Z
TLE epoch observation values (Epoch: 2026-11-03T04:12:34.624Z)
Latitude
-0.00006°
Longitude
-82.5825°
Altitude
507.581 km
Speed
7.608 km/s
True Right ascension
01h 32m 00s
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
14:45:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.566 km
Perigee altitude
494.135 km
Semi-major axis
6,875.988 km
Eccentricity
0.00054
Inclination
97.387°
RAAN
23.0036°
Arg. of periapsis
194.5655°
True anomaly
165.55805°
Mean anomaly
165.5426°
Eccentric anomaly
165.55033°
Mean motion
3.80663 °/min
Orbital period
94.57 mins
BSTAR
0.000078957
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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.FOSSASAT2E18 (TAT-A) 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-03 18:58:31.631Z | 332.714° NNW | 2026-11-03 19:00:31.631Z | 297.349° NW | 18.558° | 2026-11-03 19:02:31.631Z | 257.36° W |
| 6 mins | 2026-11-04 05:35:31.631Z | 191.648° SSW | 2026-11-04 05:38:31.631Z | 285.435° WNW | 44.149° | 2026-11-04 05:41:31.631Z | 335.436° NNW |
| 5 mins | 2026-11-04 18:39:31.631Z | 338.592° N | 2026-11-04 18:41:31.631Z | 288.98° WNW | 31.05° | 2026-11-04 18:44:31.631Z | 227.199° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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