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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Edit Public Description
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: 11 hours ago
TLE from 11 hours ago
0 FOSSASAT2E18 (TAT-A)
1 62686U 25009CF 25340.16703554 .00006118 00000-0 28992-3 0 9998
2 62686 97.4166 56.9580 0004799 298.8083 61.2669 15.19659193 49364Epoch: 2025-12-06T04:00Z
TLE epoch observation values (Epoch: 2025-12-06T04:00:31.870Z)
Latitude
-0.00011°
Longitude
-78.37344°
Altitude
508.372 km
Speed
7.611 km/s
True Right ascension
03h 47m 49s
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
12:59:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.139 km
Perigee altitude
500.534 km
Semi-major axis
6,881.974 km
Eccentricity
0.00048
Inclination
97.4166°
RAAN
56.958°
Arg. of periapsis
298.8083°
True anomaly
61.31514°
Mean anomaly
61.2669°
Eccentric anomaly
61.29102°
Mean motion
3.80166 °/min
Orbital period
94.7 mins
BSTAR
0.00028992
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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
Loading observer location...
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 | 2025-12-06 17:14:15.616Z | 57.784° ENE | 2025-12-06 17:16:15.616Z | 93.758° ESE | 16.227° | 2025-12-06 17:18:15.616Z | 129.678° SE |
| 5 mins | 2025-12-06 18:48:15.616Z | 334.548° NNW | 2025-12-06 18:50:15.616Z | 285.513° WNW | 25.448° | 2025-12-06 18:53:15.616Z | 229.255° WSW |
| 5 mins | 2025-12-07 05:26:15.616Z | 176.388° S | 2025-12-07 05:28:15.616Z | 280.15° WNW | 43.987° | 2025-12-07 05:31:15.616Z | 343.894° 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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