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 26259.33477937 .00006257 00000-0 28958-3 0 9998
2 68416 97.4649 216.8858 0001541 20.8723 339.2575 15.20481180 25794Epoch: 2026-09-16T08:02Z
TLE epoch observation values (Epoch: 2026-09-16T08:02:04.937Z)
Latitude
-0.00002°
Longitude
101.07738°
Altitude
506.485 km
Speed
7.611 km/s
True Right ascension
14h 27m 32s
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
03:01:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.416 km
Perigee altitude
500.296 km
Semi-major axis
6,879.493 km
Eccentricity
0.00015
Inclination
97.4649°
RAAN
216.8858°
Arg. of periapsis
20.8723°
True anomaly
339.25124°
Mean anomaly
339.2575°
Eccentric anomaly
339.25437°
Mean motion
3.80372 °/min
Orbital period
94.64 mins
BSTAR
0.00028958
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-17 20:31:48.850Z | 95.639° ESE | 2026-09-17 20:32:48.850Z | 73.393° E | 21.098° | 2026-09-17 20:35:48.850Z | 19.281° NNE |
| 4 mins | 2026-09-17 22:04:48.850Z | 224.172° SW | 2026-09-17 22:06:48.850Z | 267.888° W | 22.814° | 2026-09-17 22:08:48.850Z | 308.652° NW |
| 5 mins | 2026-09-18 09:34:48.850Z | 46.463° ENE | 2026-09-18 09:36:48.850Z | 94.194° ESE | 30.015° | 2026-09-18 09:39:48.850Z | 156.868° SSE |
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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