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: 1 day ago
TLE from 1 day ago
0 OPTISAT
1 68418U 26067C 26307.38772194 .00003177 00000-0 15066-3 0 9996
2 68418 97.4780 264.4307 0003198 132.2881 227.8626 15.20011110 33085Epoch: 2026-11-03T09:18Z
TLE epoch observation values (Epoch: 2026-11-03T09:18:19.175Z)
Latitude
0.00002°
Longitude
82.19969°
Altitude
510.373 km
Speed
7.608 km/s
True Right ascension
17h 37m 43s
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
13:28:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.976 km
Perigee altitude
500.575 km
Semi-major axis
6,880.913 km
Eccentricity
0.00032
Inclination
97.478°
RAAN
264.4307°
Arg. of periapsis
132.2881°
True anomaly
227.83543°
Mean anomaly
227.8626°
Eccentric anomaly
227.84902°
Mean motion
3.80254 °/min
Orbital period
94.67 mins
BSTAR
0.00015066
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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 | 2026-11-04 21:47:21.328Z | 210.617° SW | 2026-11-04 21:49:21.328Z | 278.537° WNW | 37.4° | 2026-11-04 21:52:21.328Z | 331.342° NNW |
| 4 mins | 2026-11-05 10:51:21.328Z | 332.301° NNW | 2026-11-05 10:53:21.328Z | 284.711° WNW | 26.252° | 2026-11-05 10:55:21.328Z | 241.565° WSW |
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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