VIREON-1, 68434
Orbit data source: Space-Track
VIREON-1, 68434 is a payload satellite owned by AAC ClydeSpace (UK) 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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68434 intel report (Beta)
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Identifier
Orbit
Country
UKRelated business
Manufacturer
AAC ClydeSpace
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 16U EPIC, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 VIREON-1
1 68434U 26067U 26263.45161203 .00002007 00000-0 98853-4 0 9993
2 68434 97.4697 220.8137 0002470 50.2180 309.9271 15.19114629 26403Epoch: 2026-09-20T10:50Z
TLE epoch observation values (Epoch: 2026-09-20T10:50:19.279Z)
Latitude
-0.00009°
Longitude
58.88778°
Altitude
510.511 km
Speed
7.609 km/s
True Right ascension
14h 43m 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
18:55:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.185 km
Perigee altitude
503.785 km
Semi-major axis
6,883.622 km
Eccentricity
0.00025
Inclination
97.4697°
RAAN
220.8137°
Arg. of periapsis
50.218°
True anomaly
309.90539°
Mean anomaly
309.9271°
Eccentric anomaly
309.91625°
Mean motion
3.8003 °/min
Orbital period
94.73 mins
BSTAR
0.000098853
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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.VIREON-1 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 | 2026-09-21 09:32:06.900Z | 35.122° NE | 2026-09-21 09:35:06.900Z | 89.633° E | 29.139° | 2026-09-21 09:38:06.900Z | 154.627° SSE |
| 5 mins | 2026-09-21 21:45:06.900Z | 200.656° SSW | 2026-09-21 21:47:06.900Z | 249.306° W | 38.475° | 2026-09-21 21:50:06.900Z | 326.71° 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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