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 spacecraft
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 OPTISAT
1 68418U 26067C 26171.40146383 .00003839 00000-0 18695-3 0 9999
2 68418 97.4586 129.9417 0000629 328.4245 31.6951 15.18961046 12432Epoch: 2026-06-20T09:38Z
TLE epoch observation values (Epoch: 2026-06-20T09:38:06.474Z)
Latitude
-0.00011°
Longitude
76.79813°
Altitude
511.698 km
Speed
7.608 km/s
True Right ascension
08h 39m 46s
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
07:13:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.382 km
Perigee altitude
505.516 km
Semi-major axis
6,884.086 km
Eccentricity
0.00006
Inclination
97.4586°
RAAN
129.9417°
Arg. of periapsis
328.4245°
True anomaly
31.69889°
Mean anomaly
31.6951°
Eccentric anomaly
31.69699°
Mean motion
3.79991 °/min
Orbital period
94.74 mins
BSTAR
0.00018695
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-20 20:50:32.313Z | 135.05° SSE | 2026-06-20 20:53:32.313Z | 54.632° ENE | 30.534° | 2026-06-20 20:55:32.313Z | 11.988° NNE |
| 6 mins | 2026-06-21 09:55:32.313Z | 24.946° NE | 2026-06-21 09:57:32.313Z | 68.39° E | 39.412° | 2026-06-21 10:01:32.313Z | 181.131° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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