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: 17 hours ago
TLE from 17 hours ago
0 ERMIS3
1 68425U 26067K 26308.12733410 .00003565 00000-0 16810-3 0 9994
2 68425 97.4774 265.1337 0001880 128.9645 231.1758 15.20125564 33198Epoch: 2026-11-04T03:03Z
TLE epoch observation values (Epoch: 2026-11-04T03:03:21.666Z)
Latitude
0.00002°
Longitude
175.91331°
Altitude
509.362 km
Speed
7.609 km/s
True Right ascension
17h 40m 32s
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
15:33:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.724 km
Perigee altitude
501.137 km
Semi-major axis
6,880.567 km
Eccentricity
0.00019
Inclination
97.4774°
RAAN
265.1337°
Arg. of periapsis
128.9645°
True anomaly
231.15902°
Mean anomaly
231.1758°
Eccentric anomaly
231.16741°
Mean motion
3.80283 °/min
Orbital period
94.67 mins
BSTAR
0.0001681
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-04 20:34:42.018Z | 119.394° SE | 2026-11-04 20:37:42.018Z | 58.376° ENE | 22.801° | 2026-11-04 20:39:42.018Z | 21.859° NNE |
| 4 mins | 2026-11-04 22:09:42.018Z | 236.237° WSW | 2026-11-04 22:10:42.018Z | 257.495° W | 20.493° | 2026-11-04 22:13:42.018Z | 313.642° NW |
| 5 mins | 2026-11-05 09:39:42.018Z | 49.793° ENE | 2026-11-05 09:41:42.018Z | 108.837° ESE | 32.935° | 2026-11-05 09:44:42.018Z | 163.343° S |
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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