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, 0.4 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 FOSSASAT2E20 (TAT-O)
1 63003U 25009DN 26079.45433173 .00009778 00000-0 36825-3 0 9990
2 63003 97.3221 156.8330 0001606 284.4429 75.6632 15.27295568122958Epoch: 2026-03-20T10:54Z
TLE epoch observation values (Epoch: 2026-03-20T10:54:14.261Z)
Latitude
-0.00003°
Longitude
175.28442°
Altitude
486.731 km
Speed
7.622 km/s
True Right ascension
10h 27m 19s
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
15:54:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
481.955 km
Perigee altitude
479.752 km
Semi-major axis
6,858.99 km
Eccentricity
0.00016
Inclination
97.3221°
RAAN
156.833°
Arg. of periapsis
284.4429°
True anomaly
75.68103°
Mean anomaly
75.6632°
Eccentric anomaly
75.67212°
Mean motion
3.82079 °/min
Orbital period
94.22 mins
BSTAR
0.00036825
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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 | 2026-03-21 17:20:35.938Z | 36.449° NE | 2026-03-21 17:23:35.938Z | 94.38° ESE | 24.699° | 2026-03-21 17:26:35.938Z | 155.445° SSE |
| 5 mins | 2026-03-22 05:29:35.938Z | 194.669° SSW | 2026-03-22 05:31:35.938Z | 246.309° WSW | 34.754° | 2026-03-22 05:34:35.938Z | 331.061° NNW |
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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