FOSSASAT2E19 (TAT-E), 62676
Orbit data source: Space-Track
FOSSASAT2E19 (TAT-E), 62676 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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62676 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, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 FOSSASAT2E19 (TAT-E)
1 62676U 25009BV 25286.15272844 .00005740 00000-0 27637-3 0 9993
2 62676 97.4180 3.8601 0006927 117.7125 242.4813 15.19126239 41169Epoch: 2025-10-13T03:39Z
TLE epoch observation values (Epoch: 2025-10-13T03:39:55.737Z)
Latitude
-0.00001°
Longitude
-73.08174°
Altitude
513.776 km
Speed
7.606 km/s
True Right ascension
00h 15m 26s
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
510.216 km
Perigee altitude
500.679 km
Semi-major axis
6,883.585 km
Eccentricity
0.00069
Inclination
97.418°
RAAN
3.8601°
Arg. of periapsis
117.7125°
True anomaly
242.41093°
Mean anomaly
242.4813°
Eccentric anomaly
242.44611°
Mean motion
3.80033 °/min
Orbital period
94.73 mins
BSTAR
0.00027637
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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.FOSSASAT2E19 (TAT-E) 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 05:05:16.177Z | 151.49° SSE | 2025-10-14 05:08:16.177Z | 79.265° E | 39.699° | 2025-10-14 05:11:16.177Z | 359.29° N |
| 5 mins | 2025-10-14 18:11:16.177Z | 12.067° NNE | 2025-10-14 18:13:16.177Z | 194.168° SSW | 44.66° | 2025-10-14 18:16:16.177Z | 193.074° 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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