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: 7 hours ago
TLE from 7 hours ago
0 OPTISAT
1 68418U 26067C 26263.14464531 .00003254 00000-0 15567-3 0 9996
2 68418 97.4690 220.6108 0002046 14.6357 345.4936 15.19687369 26367Epoch: 2026-09-20T03:28Z
TLE epoch observation values (Epoch: 2026-09-20T03:28:17.354Z)
Latitude
-0.00011°
Longitude
169.49547°
Altitude
508.509 km
Speed
7.61 km/s
True Right ascension
14h 42m 26s
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
03:11:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.162 km
Perigee altitude
502.346 km
Semi-major axis
6,881.891 km
Eccentricity
0.0002
Inclination
97.469°
RAAN
220.6108°
Arg. of periapsis
14.6357°
True anomaly
345.48773°
Mean anomaly
345.4936°
Eccentric anomaly
345.49066°
Mean motion
3.80173 °/min
Orbital period
94.69 mins
BSTAR
0.00015567
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-20 10:20:54.790Z | 3.576° NNE | 2026-09-20 10:23:54.790Z | 308.225° NW | 58.783° | 2026-09-20 10:26:54.790Z | 207.379° SW |
| 5 mins | 2026-09-20 20:59:54.790Z | 140.147° SSE | 2026-09-20 21:01:54.790Z | 83.863° E | 47.767° | 2026-09-20 21:04:54.790Z | 3.296° NNE |
| 6 mins | 2026-09-21 10:03:54.790Z | 16.62° NNE | 2026-09-21 10:06:54.790Z | 149.597° SSE | 70.997° | 2026-09-21 10:09:54.790Z | 187.833° SSW |
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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