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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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: 6 hours ago
TLE from 6 hours ago
0 FOSSASAT2E20 (TAT-O)
1 63003U 25009DN 26307.53794905 .00009326 00000-0 29553-3 0 9995
2 63003 97.3044 21.4686 0003043 162.2010 197.9339 15.32933092157832Epoch: 2026-11-03T12:54Z
TLE epoch observation values (Epoch: 2026-11-03T12:54:38.797Z)
Latitude
-0.00011°
Longitude
145.00778°
Altitude
472.16 km
Speed
7.629 km/s
True Right ascension
01h 25m 52s
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
14:44:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.093 km
Perigee altitude
461.929 km
Semi-major axis
6,842.148 km
Eccentricity
0.0003
Inclination
97.3044°
RAAN
21.4686°
Arg. of periapsis
162.201°
True anomaly
197.92317°
Mean anomaly
197.9339°
Eccentric anomaly
197.92853°
Mean motion
3.8349 °/min
Orbital period
93.87 mins
BSTAR
0.00029553
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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 | 2026-11-04 04:42:36.127Z | 139.926° SSE | 2026-11-04 04:45:36.127Z | 64.981° ENE | 38.078° | 2026-11-04 04:48:36.127Z | 4.902° NNE |
| 5 mins | 2026-11-04 17:41:36.127Z | 35.811° NE | 2026-11-04 17:43:36.127Z | 124.569° SE | 48.109° | 2026-11-04 17:46:36.127Z | 176.975° S |
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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