OPTISAT, 68418
Orbit data source: Space-Track
OPTISAT, 68418 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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68418 intel report (Beta)
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Identifier
Orbit
Country
GR / GRECRelated business
Manufacturer
PLANH
Mission
Operational Commercial Technology
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 OPTISAT
1 68418U 26067C 26217.37719357 .00003736 00000-0 17992-3 0 9998
2 68418 97.4618 175.3513 0004222 107.4653 252.7044 15.19357812 19416Epoch: 2026-08-05T09:03Z
TLE epoch observation values (Epoch: 2026-08-05T09:03:09.524Z)
Latitude
0.00004°
Longitude
85.62914°
Altitude
511.734 km
Speed
7.607 km/s
True Right ascension
11h 41m 24s
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
12:35:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.655 km
Perigee altitude
501.843 km
Semi-major axis
6,882.886 km
Eccentricity
0.00042
Inclination
97.4618°
RAAN
175.3513°
Arg. of periapsis
107.4653°
True anomaly
252.65821°
Mean anomaly
252.7044°
Eccentric anomaly
252.68131°
Mean motion
3.80091 °/min
Orbital period
94.71 mins
BSTAR
0.00017992
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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.OPTISAT 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 | 2026-08-06 09:20:49.284Z | 54.663° ENE | 2026-08-06 09:22:49.284Z | 94.675° ESE | 19.44° | 2026-08-06 09:24:49.284Z | 134.902° SE |
| 4 mins | 2026-08-06 10:54:49.284Z | 329.752° NNW | 2026-08-06 10:56:49.284Z | 285.606° WNW | 21.314° | 2026-08-06 10:58:49.284Z | 245.338° WSW |
| 5 mins | 2026-08-06 21:32:49.284Z | 187.739° SSW | 2026-08-06 21:34:49.284Z | 256.323° W | 40.233° | 2026-08-06 21:37:49.284Z | 337.272° NNW |
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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