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: 11 hours ago
TLE from 11 hours ago
0 FOSSASAT2E18 (TAT-A)
1 62686U 25009CF 26261.92930658 .00002498 00000-0 11417-3 0 9993
2 62686 97.3906 338.5889 0006255 22.5180 337.6329 15.21458413 92945Epoch: 2026-09-18T22:18Z
TLE epoch observation values (Epoch: 2026-09-18T22:18:12.088Z)
Latitude
-0.00006°
Longitude
6.1934°
Altitude
500.554 km
Speed
7.616 km/s
True Right ascension
22h 34m 21s
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
01:54:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.705 km
Perigee altitude
494.103 km
Semi-major axis
6,876.541 km
Eccentricity
0.00063
Inclination
97.3906°
RAAN
338.5889°
Arg. of periapsis
22.518°
True anomaly
337.6056°
Mean anomaly
337.6329°
Eccentric anomaly
337.61925°
Mean motion
3.80617 °/min
Orbital period
94.58 mins
BSTAR
0.00011417
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-19 17:48:00.010Z | 22.082° NNE | 2026-09-19 17:52:00.010Z | 128.103° SE | 48.931° | 2026-09-19 17:55:00.010Z | 177.057° S |
| 4 mins | 2026-09-20 04:27:00.010Z | 107.37° ESE | 2026-09-20 04:29:00.010Z | 66.417° ENE | 20.399° | 2026-09-20 04:31:00.010Z | 27.946° NE |
| 4 mins | 2026-09-20 06:01:00.010Z | 229.328° WSW | 2026-09-20 06:03:00.010Z | 276.958° WNW | 22.559° | 2026-09-20 06:05:00.010Z | 313.729° NW |
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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