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, 0.4 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 FOSSASAT2E18 (TAT-A)
1 62686U 25009CF 26215.95406751 .00002409 00000-0 11082-3 0 9997
2 62686 97.3950 293.4438 0006667 155.6544 204.5008 15.21271292 85959Epoch: 2026-08-03T22:53Z
TLE epoch observation values (Epoch: 2026-08-03T22:53:51.432Z)
Latitude
-0.00005°
Longitude
-2.55026°
Altitude
509.273 km
Speed
7.607 km/s
True Right ascension
19h 33m 46s
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
17:48:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.554 km
Perigee altitude
494.384 km
Semi-major axis
6,877.106 km
Eccentricity
0.00067
Inclination
97.395°
RAAN
293.4438°
Arg. of periapsis
155.6544°
True anomaly
204.46914°
Mean anomaly
204.5008°
Eccentric anomaly
204.48497°
Mean motion
3.8057 °/min
Orbital period
94.59 mins
BSTAR
0.00011082
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-05 05:01:26.589Z | 150.296° SSE | 2026-08-05 05:04:26.589Z | 61.544° ENE | 39.281° | 2026-08-05 05:07:26.589Z | 358.501° N |
| 6 mins | 2026-08-05 18:05:26.589Z | 13.002° NNE | 2026-08-05 18:08:26.589Z | 186.423° SSW | 42.409° | 2026-08-05 18:11:26.589Z | 192.015° SSW |
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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