FOSSASAT2E25, 68478
Orbit data source: Space-Track
FOSSASAT2E25, 68478 is a payload satellite owned by Fossa Systems (ES) in SSO that was launched on Mon, 30 Mar 2026 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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68478 intel report (Beta)
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Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
Fossa Systems
Mission
Operational spacecraft
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 FOSSASAT2E25
1 68478U 26067BQ 26171.31651883 .00000514 00000-0 56024-4 0 9997
2 68478 97.7599 129.5630 0000344 312.9158 47.2032 14.92139606 12199Epoch: 2026-06-20T07:35Z
TLE epoch observation values (Epoch: 2026-06-20T07:35:47.226Z)
Latitude
-0.00006°
Longitude
107.08334°
Altitude
594.145 km
Speed
7.563 km/s
True Right ascension
08h 38m 15s
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
15:45:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.523 km
Perigee altitude
588.044 km
Semi-major axis
6,966.421 km
Eccentricity
0.00003
Inclination
97.7599°
RAAN
129.563°
Arg. of periapsis
312.9158°
True anomaly
47.20609°
Mean anomaly
47.2032°
Eccentric anomaly
47.20465°
Mean motion
3.73275 °/min
Orbital period
96.44 mins
BSTAR
0.000056024
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Other satellites on launch #67 in the year 2026 (2026-03-30 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.FOSSASAT2E25 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-22 10:02:56.784Z | 14.596° NNE | 2026-06-22 10:06:56.784Z | 142.391° SSE | 44.441° | 2026-06-22 10:09:56.784Z | 189.333° SSW |
| 6 mins | 2026-06-22 20:53:56.784Z | 138.722° SSE | 2026-06-22 20:55:56.784Z | 93.62° ESE | 36.063° | 2026-06-22 20:59:56.784Z | 0.776° NNE |
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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