PEAKSAT, 68416
Orbit data source: Space-Track
PEAKSAT, 68416 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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68416 intel report (Beta)
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Identifier
Orbit
Country
GR / GRECRelated business
Manufacturer
AUTH
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
~5 kg wet, ~5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 PEAKSAT
1 68416U 26067A 26262.62527937 .00004903 00000-0 22743-3 0 9992
2 68416 97.4650 220.1444 0001152 15.6469 344.4802 15.20512338 26299Epoch: 2026-09-19T15:00Z
TLE epoch observation values (Epoch: 2026-09-19T15:00:24.137Z)
Latitude
0°
Longitude
-3.4873°
Altitude
506.619 km
Speed
7.611 km/s
True Right ascension
14h 40m 34s
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
07:42:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.054 km
Perigee altitude
500.469 km
Semi-major axis
6,879.399 km
Eccentricity
0.00012
Inclination
97.465°
RAAN
220.1444°
Arg. of periapsis
15.6469°
True anomaly
344.47667°
Mean anomaly
344.4802°
Eccentric anomaly
344.47843°
Mean motion
3.8038 °/min
Orbital period
94.64 mins
BSTAR
0.00022743
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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.PEAKSAT 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-20 21:08:08.467Z | 157.145° SSE | 2026-09-20 21:11:08.467Z | 118.837° SE | 57.446° | 2026-09-20 21:15:08.467Z | 354.445° N |
| 6 mins | 2026-09-21 10:13:08.467Z | 8.695° NNE | 2026-09-21 10:16:08.467Z | 219.533° SW | 69.123° | 2026-09-21 10:19:08.467Z | 196.755° 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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