Showing default

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.

Loading next visibility...
Identifier
68421, 2026-067F
Orbit
SSO
Country
Flag of UKUK
Related business
Manufacturer
AAC ClydeSpace
Mission
Operational spacecraft
Bus & Motor
CUBESAT 16U EPIC, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
2026-03-30 (2 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 week ago

TLE from 1 week ago
0 VIREON-2
1 68421U 26067F   26153.81780524  .00004516  00000-0  22089-3 0  9994
2 68421  97.4517 112.5162 0001150  67.4672 292.6684 15.18711797  9769
Epoch: 2026-06-02T19:37Z
TLE epoch observation values (Epoch: 2026-06-02T19:37:38.372Z)
Latitude
-0.00003°
Longitude
-73.17901°
Altitude
512.515 km
Speed
7.608 km/s
True Right ascension
07h 30m 03s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
12:50:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.494 km
Perigee altitude
505.911 km
Semi-major axis
6,884.839 km
Eccentricity
0.00012
Inclination
97.4517°
RAAN
112.5162°
Arg. of periapsis
67.4672°
True anomaly
292.65624°
Mean anomaly
292.6684°
Eccentric anomaly
292.66232°
Mean motion
3.79929 °/min
Orbital period
94.75 mins
BSTAR
0.00022089
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|