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ERMIS3, 68425

Orbit data source: Space-Track

ERMIS3, 68425 is a Greek payload satellite 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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Identifier
68425, 2026-067K
Orbit
SSO
Country
Flag of GRGR / GREC
Related business
Manufacturer
NKUA
Mission
Operational Amateur Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
2026-03-30 (4 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 ERMIS3
1 68425U 26067K   26219.83073967  .00003287  00000-0  15884-3 0  9998
2 68425  97.4617 177.7431 0003115 115.5460 244.6097 15.19325430 19783
Epoch: 2026-08-07T19:56Z
TLE epoch observation values (Epoch: 2026-08-07T19:56:15.907Z)
Latitude
-0.00002°
Longitude
-77.67398°
Altitude
511.886 km
Speed
7.607 km/s
True Right ascension
11h 50m 58s
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
23:42:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.991 km
Perigee altitude
502.703 km
Semi-major axis
6,882.984 km
Eccentricity
0.00031
Inclination
97.4617°
RAAN
177.7431°
Arg. of periapsis
115.546°
True anomaly
244.57746°
Mean anomaly
244.6097°
Eccentric anomaly
244.59358°
Mean motion
3.80083 °/min
Orbital period
94.72 mins
BSTAR
0.00015884
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