FOSSASAT2E20 (TAT-O), 63003
Orbit data source: Space-Track
FOSSASAT2E20 (TAT-O), 63003 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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63003 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: 13 hours ago
TLE from 13 hours ago
0 FOSSASAT2E20 (TAT-O)
1 63003U 25009DN 25286.47290978 .00020439 00000-0 90434-3 0 9998
2 63003 97.3441 2.1506 0004663 118.2002 241.9705 15.21691948 98886Epoch: 2025-10-13T11:20Z
TLE epoch observation values (Epoch: 2025-10-13T11:20:59.404Z)
Latitude
-0.00005°
Longitude
169.62789°
Altitude
505.34 km
Speed
7.611 km/s
True Right ascension
00h 08m 36s
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
18:49:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.904 km
Perigee altitude
494.492 km
Semi-major axis
6,875.835 km
Eccentricity
0.00047
Inclination
97.3441°
RAAN
2.1506°
Arg. of periapsis
118.2002°
True anomaly
241.92335°
Mean anomaly
241.9705°
Eccentric anomaly
241.94692°
Mean motion
3.80676 °/min
Orbital period
94.57 mins
BSTAR
0.00090434
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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.FOSSASAT2E20 (TAT-O) 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 | 2025-10-14 04:50:16.234Z | 145.284° SSE | 2025-10-14 04:53:16.234Z | 82.856° E | 34.835° | 2025-10-14 04:56:16.234Z | 4.945° NNE |
| 6 mins | 2025-10-14 17:54:16.234Z | 18.993° NNE | 2025-10-14 17:57:16.234Z | 146.746° SSE | 41.711° | 2025-10-14 18:00:16.234Z | 185.346° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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