ERMIS2, 68420
Orbit data source: Space-Track
ERMIS2, 68420 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
Orbit
Country
GR / GRECRelated business
Manufacturer
NKUA
Mission
Operational Amateur Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 ERMIS2
1 68420U 26067E 26263.11583934 .00006956 00000-0 31430-3 0 9994
2 68420 97.4569 220.5564 0001037 72.9902 287.1448 15.21267388 26371Epoch: 2026-09-20T02:46Z
TLE epoch observation values (Epoch: 2026-09-20T02:46:48.518Z)
Latitude
0.00002°
Longitude
179.83959°
Altitude
504.897 km
Speed
7.612 km/s
True Right ascension
14h 42m 13s
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
08:43:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.696 km
Perigee altitude
498.27 km
Semi-major axis
6,877.12 km
Eccentricity
0.0001
Inclination
97.4569°
RAAN
220.5564°
Arg. of periapsis
72.9902°
True anomaly
287.13344°
Mean anomaly
287.1448°
Eccentric anomaly
287.13912°
Mean motion
3.80569 °/min
Orbital period
94.6 mins
BSTAR
0.0003143
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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.ERMIS2 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-20 20:18:16.721Z | 100.439° ESE | 2026-09-20 20:20:16.721Z | 65.782° ENE | 15.271° | 2026-09-20 20:22:16.721Z | 32.131° NE |
| 4 mins | 2026-09-20 21:52:16.721Z | 220.586° SW | 2026-09-20 21:53:16.721Z | 247.794° W | 31.549° | 2026-09-20 21:56:16.721Z | 321.47° NNW |
| 4 mins | 2026-09-21 09:22:16.721Z | 66.736° ENE | 2026-09-21 09:23:16.721Z | 88.383° E | 20.68° | 2026-09-21 09:26:16.721Z | 144.335° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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