VIREON-2, 68421
Orbit data source: Space-Track
VIREON-2, 68421 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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68421 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: 12 hours ago
TLE from 12 hours ago
0 VIREON-2
1 68421U 26067F 26217.45490332 .00001971 00000-0 96996-4 0 9991
2 68421 97.4555 175.2909 0002995 85.6901 274.4675 15.19160169 19425Epoch: 2026-08-05T10:55Z
TLE epoch observation values (Epoch: 2026-08-05T10:55:03.646Z)
Latitude
-0.00012°
Longitude
57.51666°
Altitude
511.305 km
Speed
7.608 km/s
True Right ascension
11h 41m 09s
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
12:36:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.408 km
Perigee altitude
503.285 km
Semi-major axis
6,883.484 km
Eccentricity
0.0003
Inclination
97.4555°
RAAN
175.2909°
Arg. of periapsis
85.6901°
True anomaly
274.43328°
Mean anomaly
274.4675°
Eccentric anomaly
274.45039°
Mean motion
3.80041 °/min
Orbital period
94.73 mins
BSTAR
0.000096996
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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-2 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 | 2026-08-06 09:36:38.168Z | 31.365° NE | 2026-08-06 09:39:38.168Z | 84.987° E | 28.716° | 2026-08-06 09:42:38.168Z | 158.471° S |
| 4 mins | 2026-08-06 21:50:38.168Z | 219.895° SW | 2026-08-06 21:51:38.168Z | 247.246° WSW | 27.969° | 2026-08-06 21:54:38.168Z | 321.734° 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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