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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68425 intel report (Beta)
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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: 14 hours ago
TLE from 14 hours ago
0 ERMIS3
1 68425U 26067K 26197.43637927 .00003443 00000-0 16737-3 0 9993
2 68425 97.4604 155.6195 0001408 140.2161 219.9177 15.19094510 16386Epoch: 2026-07-16T10:28Z
TLE epoch observation values (Epoch: 2026-07-16T10:28:23.168Z)
Latitude
-0.00004°
Longitude
64.24511°
Altitude
512.407 km
Speed
7.607 km/s
True Right ascension
10h 22m 28s
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
12:43:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.515 km
Perigee altitude
504.576 km
Semi-major axis
6,883.682 km
Eccentricity
0.00014
Inclination
97.4604°
RAAN
155.6195°
Arg. of periapsis
140.2161°
True anomaly
219.90735°
Mean anomaly
219.9177°
Eccentric anomaly
219.91252°
Mean motion
3.80025 °/min
Orbital period
94.73 mins
BSTAR
0.00016737
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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.ERMIS3 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 | 2026-07-17 09:11:26.392Z | 57.175° ENE | 2026-07-17 09:13:26.392Z | 92.093° ESE | 15.653° | 2026-07-17 09:15:26.392Z | 127.92° SE |
| 5 mins | 2026-07-17 10:45:26.392Z | 337.107° NNW | 2026-07-17 10:47:26.392Z | 289.201° WNW | 26.064° | 2026-07-17 10:50:26.392Z | 229.318° WSW |
| 5 mins | 2026-07-17 21:23:26.392Z | 174.004° S | 2026-07-17 21:25:26.392Z | 211.035° SW | 43.55° | 2026-07-17 21:28:26.392Z | 343.627° N |
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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